Guide to the NACA Ames Aeronautical Laboratory Records at NARA San Francisco, 1939-1958

Original NARA finding aid adapted by the NASA Ames History Office staff; machine-readable finding aid created by Gabriela A. Montoya
NASA Ames Research Center History Office
Mail Stop 207-1
Moffett Field, California 94035
©1998
NASA Ames Research Center. All rights reserved.

Guide to the NACA Ames Aeronautical Laboratory Records at NARA San Francisco, 1939-1958

Collection number: Record Group 255.4.1

NASA Ames Research Center History Office

Contact Information:

  • National Archives and Records Administration, Pacific Region, at San Francisco
  • 1000 Commodore Drive
  • San Bruno, California 94066-2350
  • Phone: (650) 876-9009
  • Email: archives@sanbruno.nara.gov
  • URL: http://www.archives.gov/san-francisco/

Finding aid authored by:

  • NASA Ames Research Center History Office
  • URL: http://history.arc.nasa.gov
Date Completed:
September 1998
Encoded by:
Gabriela A. Montoya
©1998 NASA Ames Research Center. All rights reserved.

Descriptive Summary

Title: NACA Ames Aeronautical Laboratory Records at NARA San Francisco
Date (inclusive): 1939-1958
Collection Number: Record Group 255.4.1
Creator: National Advisory Committee on Aeronautics, Ames Aeronautical Laboratory; National Aeronautics and Space Administration, Ames Research Center
Extent: Number of containers: 791 boxes

Volume: 250 linear feet
Repository: National Archives and Records Administration, Pacific Region, at San Francisco.
San Bruno, California 94066-2350
Language: English.

Administrative Information

Access

Collection is open for research.

Publication Rights

Copyright does not apply to United States government records. For non-government material, researcher must contact the original creator.

Preferred Citation

[Identification of item], RG 255.4.1, NACA Ames Aeronautical Laboratory Records, Container number, Folder title, National Archives and Records Administration, Pacific Region (San Francisco), San Bruno, California.

Administrative History

The Ames Aeronautical Laboratory was the second laboratory of the National Advisory Committee on Aeronautics (NACA). The NACA was created by act of Congress on March 3, 1915 and charged with the development of aeronautical research and testing facilities to improve both civil and military aviation. By 1917 the NACA had built a fully operational aeronautical research facility called the Langley Memorial Aeronautical Laboratory near Norfolk, Virginia. By 1939, American political leaders recognized that the world was heading toward war and that other nations had surpassed the United States in basic aeronautical research. NACA leaders recognized that the Langley laboratory had run out of space for new wind tunnels and was straining the electrical capacity in the area. Thus, the Roosevelt Administration forcefully endorsed a report from the NACA Special Committee on Future Research Facilities, dated December 30, 1938, that argued for the establishment of a second research installation near the West Coast aircraft manufacturers. The tentative site suggested was the U.S. Naval Air Field and Army training base at Moffett Field in Sunnyvale, California. On February 3, 1939 President Roosevelt transmitted the $10 million request to Congress for incorporation into the second deficiency bill. A stiff partisan political struggle followed, however, and it was not until August 9, 1939, that the funds were approved as a part of the third deficiency bill.
Construction of the second laboratory began on December 20, 1939, led by an elite group from Langley, whose building priorities indicated a sense of urgency: flight research building, wind funnels, the technical services facilities, and lastly the administration building. On April 18, 1940, the center was christened Ames Aeronautical Laboratory to honor Dr. Joseph Ames, the chairman of NACA from 1927 to 1939 and a staunch advocate for basic scientific research and the responsibility of the federal government in training people for it. Responsibility for organizing the center rested with the Engineer-in-Chief, Dr. Smith J. De France, served as Center Director from 1940 to 1965. Smitty DeFrance was ably assisted by John F. Parsons, his deputy in charge of administrative matters, by Harry Goett who directed low-speed wind tunnel research, and Harvey Allen who directed high-speed wind tunnel research. Allen joked in 1943 that he was actually in charge of "Theoretical Aerodynamics and Reinforced Concrete" because, in fact, the bulk of everyone's efforts at Ames was in building facilities as quickly as possible, rather than conducting research.
The first research effort at Ames involved flight test aircraft rather than wind tunnels. The Royal Air Force Bomber Command raids over Germany pointed out the need for a de-icing system to allow aircraft to fly in all types of weather. Within a year an effective hot-air de-icing system had been developed at Ames for American heavy bombers, and Ames led the development of methods to test for icing conditions in actual flight. Lewis Rodert won the 1947 Collier Trophy in recognition of the outstanding research done at Ames. Later, the knowledge of heat transfer gained in wing de-icing experiments was applied to problems of jet aircraft and missile design.
During World War II, Ames kept its wind tunnels in almost constant operation, working to improve such famous production aircraft as the P-51 Mustang and the P-38 Lightning. A complete set of wind-tunnels was available to West coast manufactures and their military customers: the smaller 1-by-3 foot tunnel that operated at supersonic speeds, to the workhorse 7-by-10 wind tunnels, to the 40-by-80 full scale wind tunnel, then the world's largest. In 1943, the Research Division was split into two divisions, one for theoretical and applied research and the other for full-scale flight investigations. In 1944, the technical service group and the technical shops were combined into the Service Division. Otherwise, Ames' organization changed little during the war years.
Ames changed more dramatically in the post-war period. In 1953, as a result of the Hoover Commission on Government Reorganization and its recommendation on establishing a uniform nomenclature for all governament agencies, sections were renamed branches, the primary operational unit below the division. Two new divisions were added at Ames: the High-Speed and Flight Research Division, and the Research Instrumentation and Engineering Services Division.
Another key addition, in 1950, was the Ames Unitary Plan Design Group. More high-speed tunnels and more sensitive instrumentation were required for the United States to compete in the world of jet aircraft and guided missiles. To combine the talents of NACA, university, military, and industry researchers--as well as to forge a unified front in lobbying for the enormous funds required--Ames led the formation of a Unitary Plan wind tunnel design group. This group was to design a series of high-speed wind tunnels located wherever such research was needed, at a total estimated cost of $10 billion. After Congress whittled down the Unitary Plan to $27 million only one such tunnel was constructed--at Ames. Not only was the tunnel itself an engineering masterwork--with three tunnels operating integrated to make the most efficient use of drive motors and researchers' time--but the tunnel supported much of the key work that led America into the space age.
By 1957, international pressures, the arms race, and the orbit of Sputnik again forced change in the administrative structure of Ames. On July 29, 1958, the National Aeronautics and Space Act was signed. On October 1, 1958, the National Aeronautics and Space Administration was born, it absorbed the NACA, and Ames became a part of America's space program.

Scope and Content

The NACA Ames records document a broad range of theoretical work, applied research, and testing related to aeronautics and space technology. Subjects include aerodynamics, airframe problems, flight simulation, instrument development, satellite re-entry, heat transfer and de-icing. It also documents design and wind tunnel testing of such aircraft as the P-51 Mustang and P-38 Lightning. Also included are records relating to project proposals and research authorizations, minutes of the NACA committees on which Ames staff served, and general administrative matters. The records are primarily central files, consisting of correspondence, data sheets, minutes of meetings, memorandums, specifications, and technical reports. Nontextual records include artwork, engineering drawings, and photographs interfiled with textual records. The general Ames photograph files are still in the Federal Record Center.

Common Abbreviations in the Ames Records

1. Branch Codes used by the Ames Report Unit

The Report Unit was the office at Ames that compiled and published technical reports. These reports were written by researchers working in the technical branches at Ames. These branches were identified by a two-letter code which often appear in the file headings for Report Unit records, as well as in the Central File records.
The two letter code mimics the organization chart at Ames. For example, every branch within the Aeronautics Division began with the letter A. The second letter identified the specific branch. The branches were usually defined as a group working with a specific tool, like a wind tunnel. More recently, the branch codes can be found in the Ames telephone directories. For the 1950s, these branch codes were used.
  • AA 7-by-10 foot Wind Tunnel Branch
  • AB 16 foot High Speed Wind Tunnel Branch
  • AC 1-by-3 foot Speed Wind Tunnel Branch
  • AD 40-by-80 foot Wind Tunnel Branch
  • AE 1-by-3 foot Supersonic Wind Tunnel
  • AF 12 foot Pressure Wind Tunnel Branch
  • AG 6-by-6 foot Supersonic Wind Tunnel Branch
  • AH Flight Research Branch
  • AK Flight Engineering Branch
  • AL Theoretical Aerodynamics Branch
  • AM Instrument Development Branch
  • AN 10-by-14 inch Supersonic Wind Tunnel Branch
  • AO Supersonic Free Flight Wind Tunnel Branch
  • AP Low Density Heat Transfer Wind Tunnel Branch
  • AQ Unitary Plan Design Group

2. NACA and NASA Report Abbreviations

The basic product of all NACA work, and to a lesser extent NASA work, was the technical report. Thus, RG255.4 contains a great many reports or draft reports, primarily in the Report Unit series but also interfiled in the Central File series. All reports were published by the Government Printing Office, and some were reprinted in scientific journals, though not all were given broad public distribution.
Each report is identified by an alpha-numeric code. The suffix is a number assigned chronologically. The prefix is a letter code (shown below) that identifies the type of report it is, and these categories have changed several times over NACA and NASA history. For a complete description of the report generation process see: Alex Roland, Model Research: The National Advisory Committee for Aeronautics, 1915-1958(NASA SP-4103, 1985) especially volume II, Appendix G "Reports." Generally, advance reports, notes, and memorandum present partial or preliminary results of a research project and are data-rich but text-light. These are intended to expedite the flow of information to NACA customers. Reports are the more formal presentation of ideas, hypotheses, and supporting data.
The report-related files in RG255.4 only occasionally hold the final published reports. Mostly they contain raw research data, drawings or photographs, draft versions, peer reviews, distribution lists, and correspondence with the printing office. Thus, researchers can always start their research into NACA reports more efficiently by finding the published report elsewhere. Reports can be found on microfiche at most federal government depository libraries (to locate the one nearest you point your browser to http://www.gpoaccess.gov/libraries.html ). NASA's technical report server (RECONselect) allows users to search NASA and NACA publications by author, title, report name, or subject heading, and the Digidocs system allows readers to download digitized versions of select NACA reports. To access the technical report server point your browser to: http://www.sti.nasa.gov/RECONselect.html . Reports can also be found at many engineering libraries or NASA Center libraries.
Prefix abbreviations for NACA reports:
  • ACR= Advance Confidential Report
  • ARR= Advance Restricted Reports
  • CMR= Confidential Memorandum Report
  • CR= Contract Report
  • CRM= Confidential Research Memorandum
  • Memo= Memorandum
  • MR= Memorandum Report
  • Rep= Report
  • RM= Research Memorandum
  • RMR= Restricted Memorandum Report
  • TM= Technical Memorandum
  • TN= Technical Note
  • TR= Technical Report
  • WR= Wartime Report

Additional Note

Filing Manual

 

Central Files, 1939-1957

Physical Description: Boxes 1-617 (207 ft.)

Scope and Content Note

Arrangement

Arranged in alpha-numeric order, according to the Central File filing manual shown in Appendix.
Records consist of administrative, budgetary and research correspondence. Most of the correspondance is between the Ames Engineer-In-Charge and NACA headquarters staff in Washington, D.C. Much of this correspondence includes letters written by Ames staff for the directors signature, or memoranda to file. Some correspondence is between Ames, Langley Field, and the Cleveland Engine Research Laboratory dealing with such research topics as wing de-icing, metallurgical problems, ballistics, equipment specifications, and airframe problems such as duct-rumbling and dive-stress. In addition, there are minutes of meetings of the NACA committees on aerodynamics, aircraft powerplants, aircraft materials and structures, and jet propulsion. Also included are communication with other governmental agencies such as the Navy and Army Air Corps, Civil Service Commision and the Civil Aeronautics Board, as well as private companies such as Chance-Vought and Gruman, with universities, and the general public.
 

Report Unit Files, 1947-1954

Physical Description: Boxes 1-100 (33 ft.)

Scope and Content Note

Arrangement

Arranged chronologically. In addition, most documents bear a letter code identifying the originating office (see Common Abbreviations in the Ames Records ), as well as the index number of the final published report.
Records consist of materials compiled by the Ames Report Unit for publication of research reports. Most of these are raw materials, peer reviews, and early draft of technical reports prepared by the following branches of Ames' Aeronautical Research Division: Theoretical and Applied Research, Full Scale and Flight Research, High Speed Research, Research Instrumentation, and the Unitary Plan Design Group.
 

Records of the Ames Unitary Plan Design Group, 1950-1953

Physical Description: Boxes 1-68 (22 ft.)

Scope and Content Note

Arrangement

Arranged by topic.
Records consist of requisitions, contracts, cost estimates and bids, progress reports, blueprints, construction specifications, memoranda, and correspondence with engineers at Langley and Lewis. The Ames Unitary Plan Design Group was created for national coordination of the unitary plan, so-called because it unified the efforts of aerospace engineers from the NACA, universities, industry, and the military services to build a series of wind tunnels in the transonic and supersonic range. These records begin with the early planning for the unitary wind tunnel system, discuss ways to pare down the plan, and culminate in the preliminary design of the single unitary plan tunnel constructed at Ames. Construction on the Ames Unitary Plan Wind Tunnel began in 1953, and it encompassed an 11-by-11 foot transonic tunnel and two supersonic tunnels of 9-by-7 feet and 8-by-7 feet.
 

Records of the Research Instrumentation Division, 1941-1956

Physical Description: Boxes 1-6 (2 ft.)

Scope and Content Note

Arrangement

Arranged alphabetically by item of equipment.
Records consist of requisitions, reports, studies, recommendations and other correspondence relating to test equipment in use, under development or requested for use at Ames. Among the items discussed are altimeters, gyroscopes, film readers, and various types of recorders.

 

Central Files, 1939-1957

Box Box 1

A1-5 Aberdeen Proving Grounds - Ballistic Res. Laboratories. 1947-1948

 

A1-10 Airfoils - General. 1947-1948

Box Box 2

A1-10 Airfoils. General. [1940-1946]

 

A1-10a Ordinator Test Results. [1942-1944]

 

A2-10 Baldwin Locomative Works. [1944-1945]

 

A3-10 Compressibility Effects. (General), [1941-1945]

Box Box 3

A3-20 Computations - General. [1941-1946]

 

A3-20 Computations - General. 1947-1948

 

A3-20a Computations - REAC. 1948

 

A4-20 Engineering Designs (General).

 

A4-20a Engineering Designs Drawings. [1941-1945]

 

A4-25 Duct Inlets (Submerged Types). [1945-1948]

Box Box 4

A5-10 Engines. [1941-1945]

 

A5-10 Engines. (1948)

 

A10-10 Jet Propulsion. [1943-1946]

 

A10-10 Jet Propulsion. (1947-1948)

Box Box 5

A12-5 Lubricants and Fuels. [1942-1946]

 

A14-5 Metals - General. [1942-1946]

 

A14-10 Missiles. (1944-1948).

 

A19-10-20b Research. Aerodynamic. - General. [1940-1945]

 

A19-10 Research - Aerodynamic - General. (1948)

 

A19-20d Research - Compressibility Effects Upon Tail Surfaces. [1941].

Box Box 6

A21-5-15 Tailess Airplanes - Reports (General). [1942-1944]

 

A21-20-24-10 Tests. Progress Reports. Water Channel. [1941-1945]

Box Box 7

A-159 (MX-583). 1944

 

A-248 Vickers-Armstrong M-235, (1948-1955)

 

A-248 Vickers-Armstrong M-235.[1948-1955]

Physical Description: Drawings Only.
 

A-1-1 A21. Effect of Leading-Edge Shock Wave on Initial Boundary-Layer Development on a Wedge. [1953-1955]

 

A-1-2 A13 Study of Nonlinear Conical Flow over Triangular Wings at Supersonic Speeds. [1951-1953]

 

A-1-2 A22 Transonic Flow Over A Curved Leading Edge. [1953-1955]

Physical Description: [2 folders]
 

A-1-4 A14 Development of Technique for Investigating Heat Transfer at Mach Numbers of the Order of 10. [1953-1956.

Physical Description: 2 folders.]
 

A-1-4 A34 Calibration of a Vortex Type True Free Air Thermometer at Transonic Mach Numbers (2x2). [1954-1955.]

 

A-2-1 A1 Investigation of the Static Stability of Swept-Back Wing and Wing-Body Combinations. [1953-1955]

Box Box 8

A-2-1 A3 Investigation of the Effects of Operating Propellers on the Aerodynamic Char. of a Swept-Wing Airplane. [1951-1954]

 

A-2-1 A5. Investigation of the Static Stability of Missiles with Wings & Tails. [1951-1955.

Physical Description: 2 folders
 

A-2-1 A8. Determination of the Effect of Wing Plan Form on Damping in Pitch. [1956]

 

A-2-1 A9. Effect of Wing Plan Form and Aircraft Configuration on Dynamic Derivations. 1954.

Physical Description: [2 folders]
 

A-2-1 A11. Search for, and Evaluation of Criteria for Satisfactory Lateral and Directional Dyn. Stability and Control. [1951-1952]

Box Box 9

A-2-1 A13. Inv. of the Rel. of Servomechanism Char. and Aircraft & Dynamic Stability Char. required for Aut. Stabil. [1954]

 

A-2-1 A14. Investigation of the Requirements of Artificial Fuel System. [1954]

 

A-2-1 A17. Wing Tunnel Investigation of the MX-656 Research Airplane. [1952-1954]

 

A-2-2 A21. Investigation of Controls for Triangular Wings. [1952]

Physical Description: [2 folders]
 

A-2-2 A22. Investigation of Controls for Wings with Large Angles of Sweep. [1951]

 

A-2-2 A23. Flight Inv. of Longitudinal and Lateral Control Char. of Fighter-Type Airplanes at Transonic Speeds. [1951]

Box Box 10

A-2-1 A31. Spersonic WT Invest. of the Control Effectivness of the Hughes MX-904 (Falcon) Missile. 1951-1953.

Physical Description: [Enclosures] (*Closed)
Box Box 11

A-2-1 A33. Stability and Control Inv. of an Infra-Red Seeking Rocket and an 8-Centimeter Oerlikon Rocket [1951-1954

Physical Description: Enclosure - USN Closed]
Box Box 12

A-2-1 A33. Sidewinger. U.S. Naval Ordinance Test Station (NOTS). [1952-56

Physical Description: Enclosures. U.S.N. Closed]
Box Box 13

A-2-1 A35. Inv. of Static Stability Character of the Lockheed XFO-1 Airplane Model at High Supersonic Speeds [1952

Physical Description: Enclosures. Closed]
 

A-2-1 A36. Free Flight Investigation of Powered Dynamic Model of the Lockheed XFO-1 Airplane [1952.

Physical Description: Closed.]
 

A-2-1 CF A41. Effect of the Tail Height on the Longitudinal Stability of a Swept-Wing Fighter Airplane [N.D.]

 

A-2-2 A39. Investigations of Supersonic Speeds of Trailing-Edge Flap Controls. 1951.

 

A-2-1 A52. Preliminary Studies of a Simple Mechanical Analogue for Evaluating the Dynamic Stability of Aircraft. [1954].

Box Box 14

A-2-1 A54. Lateral Stability Characteristics of Triangular Wings at High Subsonic and Supersonic Speed. [1954].

 

A-2-1 A60. Experimental Investigation of Horizontal Tail Hinge-Moment Characteristics of Bomarc Missile [1951-1953.

Physical Description: Closed.]
 

A-2-1 A65 Study of Coordinate System for Simplifiying the Calculations of Missile Trajectories in Three Dimensions. 1953-1954.

 

A-2-2 A67 Simulations of Lateral Oscillatory Characteristics of the Convair XB-58 (MX-1964) Airplane. (C) [1954.

Physical Description: Closed]
 

A-2-1 A72 Investigation of the Dynamic Longitudinal Stability of Bodies of Revolution.

 

A-2-1 A77 Investigation of the Stability Characteristics of the B-62 Missile (Northrop N-69). (C). [1954.

Physical Description: Closed]
 

A-2-1 A41 Stability of Bodies of Revolution at High Supersonic Speeds S/C Stability and Control. (C). [1953-1954]

 

A-2-1 A41 Drawings. F-86. 1950

 

A-2-1 A41 Drawings. F-86. 1952

 

C-F A-2-1 A44 Investigation of Ground Effect on Longitudinal Stability and Control of Low-Aspect-Ratio Airplanes. N.D.

Box Box 15

A-2-1 A91 Chance-Vought Aircraft Report #10,035. 1955.

 

A-2-1 A91 Chance-Vought Aircraft Report #10,109. 1956.

 

A-2-1 A91 Drawings Recieved. 1957.

 

A-2-1 A91 Ames 9x7 SSWT T-11. CVA Regulus II.

Physical Description: [7 Folders]
Box Box 16

A-2-1 A91 Regulus II,N.D.

Physical Description: 9x7 Drawings.
Box Box 17

A-2-1 A91 Ames 9x7 T-11. CVA Regulus II Model Photos. [1956]

Box Box 18

A-2-2 A91 9x7 Tk SSWT. Test 11. Regulus II. [Computer Print-Outs. 1956.]

Box Box 19

A-2-3 A-46 Study of the Characteristics of Airplanes in the Region of the Stall. (F-86). [1953]

 

A-2-3 A-47 Investigation of Electromagnetic Model Restrain for Dynamic Stability Tests in Wind Tunnels. 1952-1955

 

A-2-1 A44 Investigation of Ground Effect on Longitudinal Stability and Control of Low-Aspect-Ratio Airplanes

 

C-F A-2-2 A48 Evaluation of the Dynamic Stability and Control Characteristics of a Triangular Wing Airplane Design. 1952-1955.

 

A-2-2 A50 Force and Moment Measurements on the XSSM-AX23 Dart Missile. 1954.

 

A-3-1 A2 High Speed Characteristics of Scoop Inlets for Operation at Supersonic Speeds. 1953

 

A-3-1 A3 Low Speed Char. of Scoop Inlets for Operation at Supersonic Speeds. [1954]

Box Box 20

A-3-1 A8 [F-93A. Drawings. 1954]

Box Box 21

A-3-1 A8 Flight Investigations of Air-Induction Systems. [1950-1953]

Box Box 22

A-3-1 A10 Wind Tunnel Tests of Air Sampling Devices. [1952]

 

A-3-1 A12 Flight Investigation of Effects of Jet Exit Configuation on Exit Losses. (C). [1951-1954]

Box Box 23

A-3-1 A13 Supersonic Tunnel Tests of Fixed Geometry Nose Inlet for the F-100 (Sabre 45) Airplane. 1951-1954]

Physical Description: 6 x 6 [Two Folders
Box Box 24

A-3-1 A13 [Drawings for above. 1951]

Box Box 25

A-3-1 A13 [As above. 1951-1952]

Box Box 26

A-3-1 A13 [As above. 1951-1952]

 

A-3-1 A14 Investigation of F100 Nose Inlet. [1952]

Box Box 27

A-3-1 A15 Investigation of Inlets of F-104 (Lockheed L-246) Airplane. (C).1952-1955

Physical Description: 6 x 6 Wind Tunnel.
 

A-3-1 A15 LAL 218 Model Drawings (Wind Tunnel) April 27, 1953

Box Box 28

A-3-1 A15 [Loose Drawings]

Box Box 29

A-3-3 A31 Enclosures w/Shipping List. 1956-1957]

Physical Description: [Four Envelopes.
Box Box 30

A-3-3 A31 [Drawings. 1956]

Box Box 31

A-3-3 A31 [Drawings. 1956]

Box Box 32

A-3-3 A31 [Drawings. 1956]

Box Box 33

A-3-3 A31 Data Pertinent to Wind Tunnel Tests of the 0.122 Scale XSM64A Air Indution System Evaluation Model. 1957

 

A-3-3 A31 Working Papers. [1957]

 

A-3-3 A31 Structural Analysis of the XSM-64A (G-38). 122-Scale D54 Diffucer Evaluation Model. 1956]

Physical Description: [Two Folders.
Box Box 34

A-3-3 A31 Factor Board Typewriter Tabulation. Test 20. NAVA110.

Physical Description: 9 x 7.
 

A-3-3 A31 Preliminary Analysis of the Missile Plus Booster Installation. Revised. 1957

Box Box 35

A-3-3 A31 Determination of the Engine Air-Diffuser Characteristics of the NAVAHO Missile (XSM-64A). 1956

 

A-3-3 A31 Preliminary Analysis of the Missile Plus Booster Installation. 1956]

Physical Description: [Two Folders.
Box Box 36-39

A-3-3 A32 Drawings to the Above. 1956

Box Box 40

A-4-1 A1 Investigation of a Propeller-Spinner Combination. [1953]

 

A-4-1 A3 Investigation of Dual Rotating Propellers. (C). [1954]

 

A-4-1 A4 Tests of a Wide-Blade Propeller at Negative Thrust. [1954]

 

(CF) A-4-1 A5 Investigation of a Supersonic Propeller Having Blunt Trailing Edges. [1953-1955]

 

(CF) A-4-2 A2 Investigation of Wing Interference and Nacelle Interference on the First-Order Vibratory Stresses on Propeller Blades. 1951-1955

 

A-4-3 A6 Tests of Lockheed YC-130 Turbo-Propeller Installations in Ames 40-by-80 Foot Wind Tunnel. [1954]

 

A-6-2 A1 Full-Scale Tunnel Investigation of McDonnell Model 82 Convertiplane Rotor [1953]

 

A-7-1 A1 Investigation of Airfoils with Blunt Trailing Edges. [1951]

 

A-7-1 A1 Development of a Method for Estimating Three-Dimensional Data from Two Dimensional [1953]

Box Box 41

A-7-1 A41 Boundry-Layer Control Inves. with Wing and Horizontal Tail Panels. [1950-1953]

 

A-7-1 A41 [Drawings Douglas. 1950-51]

Box Box 42

A-7-1 A44 Exper. Investi. of Effects of Variation of Plan Form, Sweepback, Thickness and Camber Wings of Moderate Aspects Ratio. [1953]

 

A-7-1 A46 The Effects of Taper on the Transonic Characteristics of Airfoils. 1951-1955

 

A-7-1 A47 Summary and Analysis of Hi-Sp Airfoil Data Obtained in 1 and 3½ Hi-Sp W/T at the Ames Aero Lab. (C). [1953]

 

A-7-1 A48 Static Two-Dimensional-Airfoil Character of Transonic Spds.

 

A-7-1 A52 Experimnetal Study of Boundry-Layer Control on Triangular Wings. 1952-1955

 

A-7-1 A56 Effect of Taper Ratio and Sweep Angle on Low-Aspect-Ratio Wings at Transonic and Super-Sonic Speeds. 1953-1955

Box Box 43

A-7-2 A21 Investigation of the Interrelation of Body Shape Parameters in Determining Optimum Supersonic Bodies, [1951-1953]

 

A-7-2 A55 Supersonic Wind Tunnel Investigation of the MX-1593 Missile. USAF. (C).1954

Physical Description: 10 x 14.
 

A-7-2 A102 Investigation of Multiple Body Configurations of Termsonic + Supersonic Speeds, 1955

 

A-7-3 A31 High Speed Wind-Tunnel Investigational Aerodynomic Characteristics of XB-52 Airplane [1951-1953]

 

A-7-3 A32 Wind-Tunnel Investigation of the Aerodynamic Characteristics of the MX-656 Research Airplane at Supersonic Speeds. [1951]

Box Box 44

A-7-3 A32 W/T Investigation of the MX-656 in AMES 6 x 6. 1945-1953

Box Box 45, 46, 47

A-7-3 A32 [Dwgs w/ltr. 2-17-49

Physical Description: Blueprint]
 

A-7-3 A32 [Dwgs w/ltr. 11-1-48

Physical Description: Blueprint]
Box Box 48

A-7-3 A35 Supersonic Wind-Tunnel Investigation of MX-775A Missile. [1952]

 

A-7-3 A36 Investigation of External Stores and Nacelles on Supersonic Airplanes. [1953]

 

A-7-3 A37 Supersonic Wind-Tunnel Inv. of Aerodynamic Characteristics of Douglas XF40-1 Airplane. [1953]

 

A-7-3 A42 Effect of Vertical Position of Wing on Fuselage At Transonic and Supersonic Spds. (c). [1951]

 

A-7-3 A49 Investigation in Ames 40 x 80 W/T of Low Speed Stalling Characteristics of Republic RF-84F Airplane, (R) [1951-1952]

 

A-7-3 A50 Drag Cleanup Study on Lockheed F-94C Airplane. (C).[1952]

Physical Description: 40 x 80 WADC.
Box Box 49

A-7-3 A43 Experimental Investigation of a 0.07 - Scale Model of the XM-770 Missile. (C).1951-1952

Physical Description: 6 x6.
 

A-7-3 A43 [Drawings, Douglas, 1951]

Box Box 50

A-7-3 A51 Supersonic Wind Tunnel Tests of a Model of the Republic XF-103. Airplane (MX-1554). (C).

Physical Description: 1 x 3. WADC 6 x 6
 

A-7-3 A53 Tests of a Model of the USAF Republic XF-103 in the Ames 6-by-6 Foot Supersonic Tunnel. [1953]

 

A-7-3 A54 Tests of Wing Tip Tank with Internal Flow. (C). [1952]

Box Box 51

A-7-3 A58 Experimental Investigation of the Subsonic and Supersonic Drag and Stability of MX-1964. 1952-1956

 

A-7-3 A58 Dimensional Data Report for the 1/17 - Scale Pressure and Hinge Moment Model of Project MX-1964. Convair. 10 February 1954

 

A-7-3 A58 Addendum C [to the above]

Box Box 52

A-7-3 A58 [Drawings. 1952]

Box Box 53

A-7-3 A58 Addendum B [to demi. Report above. 2nd Copy of Demi Report MX1964]

 

A-7-3 A58 Enclosures to Convair Shipment Notice to Ames No 8904. 18 Nov 1954

Physical Description: [Drawings]
 

A-7-3 A58 Enclosure to Langley Letter to AFD Feild Report, Langley Air Force Base. January 22, 1953.

Physical Description: [Drawings]
Box Box 54

A-7-3 A59 Wind-Tunnel Investigation of Aerodynamic Characteristics of Lockheed L-246 Airplane. 1952-1956.

Box Box 55

A-7-3 A59 [Loose Drawings. 1954]

Box Box 56

A-7-3 A59 F-104. (L-246) (1953)

Box Box 57

A-7-3 A60 Tests of a Model of the USAF McDonnell XF-101A Airplane in the Ames 6-by-6 foot Supersonic Tunnel, (C). 1953-1955

Box Box 58

A-7-3 A60 [Loose Drawings and Blueprints for the F-101 8% Scale Wind Tunnel Model. 1953]

Box Box 59

RA A-7-3 A60 F-101A. McDonnell Aircraft Corp. 1952-1955.

Physical Description: [2 folders, Drawings]
Box Box 60

[As above. 1953.

Physical Description: Drawings & Blueprints.]
Box Box 61

A-7-3 A66 XF8U Chance Vought. 1953

Box Box 62

A-7-3 A66 Experimental Investig of the Drag, Stability, Inlet Characts. of the Chance Vought XF8U-1. (C) 1953-1956

Physical Description: (6-by-6-W/T)
Box Box 63

A-7-3 A66 [Loose Drawings 1953]

 

A-7-3 A72 Shock-Expansion Methods of Determining Wing-Body Interference at High Supersonic Speeds 1953-1955]

Physical Description: [Closed Folder
 

A-7-3 A78 Investigation of Aerodynamic Charact [eristics] of Complete Model (approx. 1/8 scale) XF 40-2 Airplane in 6-by 6 foot W/T. 1953-55

Box Box 64

A-7-3 A80 Ivestig of Methods of Drag Reduction for the F-102 Airplane Config. (C). 1954-1955

 

A-7-3 A82 Investigation of Performance and Aerodynamic Stability and Control of RQ-2 Drone (C) October-November 1954

Box Box 65

A-7-3 A103 Tests of Air Sampling Probe in 2 by 2 foot Tunnel.

 

A-7-4 A73 Aerodynamic Tests of Dalmo Victor Antenna AN-SPS-5A

Physical Description: [Closed Folder]
 

A-7-4 A94 Shakedown and Calibration Tests of Ames Unitary Wind Tunnel. 1955

Physical Description: [Closed Folder]
Box Box 66

A-71 15 Airplanes-Ice Research (General) 1941-1948

 

A-71 15a Airplanes-Lockheed 12 A. General. 1938-1948

Box Box 67

A-71 15b-15e Airplanes-Lockheed 12 A. [reports of inspections of aircraft specifications (15b) Maint/equip orders, problems, blueprints (15c) Radio Equip (including bid material) (15d) transmital statements (for reports) (15e) P.D. & Reports (re-thermal ice prevention (15c)]

 

AF1-15K-AF1-15-L Airplanes 0-47A. 1940-1945 [ General correspondence, shipping tickets invoices maint equipemnt and standards, orders for spares, etc.]

 

AF1-20 Airports, in Contact with 1941 [Air Corp Circular on price & location of aircraft POL; request for fuel]

 

A71-25 Air Transport Assoc of America [List of key men in Assoc; agenda for conference]

 

AF1-30 American Airlines. 1941-1946 [Correspondence between AA, CA Board and NACA re deicing problems]

 

AF1-35 & AF1-35a Army Air Forces Material Command. [General Correspondence re icing problems and suggestions.]

Box Box 68

AF2-30 British Air Commission De Icing Investigation [December 23, 1941-February 17, 1947]

 

AF3-3 Cabin Heating or Cooking. 1945-1946

 

AF3-3 Corres only re TN1682 (1948)

Physical Description: [3 folders]
 

AF3-5 Carburetor Icing Problems. August 17, 1940-June 26, 1945

 

AF3-6 Civil Aronautics Admin. April 10, 1941-August 4, 1944

 

AF3-8 Compounds and Solutions, [Weather aids] 1941-1947

 

AF3-9a Conferences Aircraft Ice Prevention Conference 1945

 

AF3-10 Consolidated and Vultee [de-icing] March 8, 1941-August 22, 1945

 

AF3-12 Contact Speed. - Alternater Drive September 8, 1944-April 9, 1946

 

AF3-15 Contact-DeIcing. General. October 17, 1940-March 1, 1941

 

AF3-15b Contracts, Drawings-Lockheed. 1941

 

AF3-15c Contracts, Lockheed 12-A. 1940-1941

 

AF3-20a Contracts. B-24. Consolidated. Deicing General. February 20, 1942-March 13, 1944

 

AF3-20a Preliminary Data Report. 26 October 1942

Box Box 69

AF3-20b [Contracts B-24 Dwgs, Supplies,] Consolidated. 1942-1943

 

AF3-20b B-24 Blueprints 1939-1942

Box Box 70

AF3-20b [Loose B-24 blueprints]

Box Box 71

AF3-20b [Loose B-24 blueprints]

Box Box 72

AF3-20b [Loose B-24 blueprints]

Box Box 73

AF3-20b [Loose B-24 blueprints]

Box Box 74

AF3-20b [Loose B-24 blueprints]

Box Box 75

AF3-20b [Loose blueprints]

Box Box 76

AF3-20b [Loose blueprints]

Box Box 77

AF3-20b [Loose blueprints]

Box Box 78

AF3-20b [Loose blueprints]

Box Box 79

AF3-20b [Loose blueprints]

 

AF3-20b [Loose blueprints]

 

AF3-20b [Loose blueprints]

Box Box 80

AF3-20b [Loose blueprints]

Box Box 81

AF3-20b [Loose blueprints]

Box Box 82

AF3-20b [Loose blueprints]

Box Box 83

AF3-20b [Loose blueprints]

Box Box 84

AF3-20b [Loose blueprints]

Box Box 85

(AF) 3-20c. Contracts. B24 Consolidated

 

AF3-20c Preliminary Results. 1943-1944

Box Box 86

(AF) 3-25a. Contracts. B17f. Boeing. October 21, 1942-July 16, 1943

Physical Description: [Drawings, Supplies, etc. Supplies, etc.]
 

(AF) 3-25b "Instructions for Operation, Inspection, and Maintenance of Thermal Ice Prevention System on B-17F"

Box Box 86

(AF) 3-25. Contracts. B-17. Boeing. 1943-1944.

 

(AF) 3-25b. Preliminary Results of Tests of Super-Charger, Excharger, Design Number 2, B-17F. January 2, 1943.

 

(AF 3-25a. BAC Standards BR. 1942-1944

Box Box 87

(AF) 3-25b P/D "Tests of Army Plate-Type Heat Exchanger, Model 1, on XB-17F" Look. August 3, 1943.

 

(AF) 3-25b Preliminary Performance Data, B-17F Thermal Ice-Prevention Equipment. Dec. 23, 1942

 

(AF) 3-25b P/D "Tests of Army Plate-Type Heat Exchanger, Model 2, on XB-17F." Selna. August 18, 1943.

 

(AF) 3-25b "Analysis of Thermal Ice - Prevention Equipment for the Boeing B-17F Airplane." November 10, 1943.

 

(AF) 3-25c P/D "Details of the XB-24F Airplane Fuselage Static Airspeed Installation." Jones and Schearer. February 25, 1943

 

(AF) 3-25c P/D "Flight Tests of thermal Ice-Prevention Equipment on XB-24F" Neel and Rodert. April 6, 1943.

Physical Description: Loose blueprints 1943
Box Box 88

(AF) 3-30 Contracts. C-46 Curtiss Wright. 1943-45 [General Correspondence, photographs of parts, loose blueprints etc.

Physical Description: 2 folders]
Box Box 89

(AF) 3-30a Contracts. C-46 Curtiss-Wright. [Drawings, Supplies, Etc. 1943-46

 

(AF) 3-30a [Loose Drawings and blueprints]

Box Box 90

(AF) 3-30a [Loose drawings and blueprints]

Box Box 91

(AF) 3-30a [Loose drawings and blueprints w/attached correspondence March 1943

Box Box 92

AF 3-30b P/D I "Flight Tests of Thermal Ice Prevention Equipment System on B-24 D Airplane" [dtd 11/20/1942.]

 

AF 3-30b Corres re only TN 1599. 1948.

 

AF 3-30b Corres re only TN 1235 1948.

 

AF 3-30b Corres re only RM A5F11 1945.

 

AF 3-30b Corres re only MR A5B15 1945.

 

AF 3-30b Corres re only MR A5E15. 1946.

 

AF 3-30b Corres re only re Rept "Measurements of Free Water in Cloud Under Conditions of Icing" (1944-1948)

 

A3-30b Corres only re RM On C-46 1945

 

AF 3-35 XC-53a. Douglas. General 1943-44

 

AF 3-40 XB-35. Northrop. General 1943-44

 

AF 3-45 Contracts. D-5. General. November 23, 1943-December 28, 1943

 

AF 3-50 Preliminary Data.

Box Box 93

AF 4-10 Douglas Aircraft Company. August 5, 1941-November 18, 1947. [Decing]

 

AF 5-5 Engine Research Laboratory (Program) Cleveland. February 7, 1944-July 25, 1945. [Deicing]

 

AF 5-10 Engine Research Tunnel. LMAL. (Ice Research) May 28, 1941-December 7, 1944.

 

AF 5-20 and AF 520a Equipment and De-Icing Specifications - General. July 9, 1941- September 17, 1946]

Physical Description: [9 folders
 

AF 5-30 Exhaust Heat De-Icing (General) September 9, 1940- August 9, 1946.

 

AF 5-40 Exhaust Heat Exchanges. July 9, 1942-May 23, 1947

Box Box 94

AF 5-40 [Loose drawings and blueprints. 1941]

 

AF 5-40 [Loose drawings and blueprints. July 1941-August 1942]

 

AF 5-40a Exhaust Heat Exchange (Airesearch Mfg. Co.) 1942-1944

 

AF 5-40b Exhaust Heat Exchangers, Wm. Chace Co. - General Plate Division July 13, 1942-September 28, 1942

Box Box 95

AF 5-40c Exhaust Air Heat Exchangers, General Electric Co. May 28, 1942-November 6, 1946

 

AF 5-40d Exhaust Air Heat Exchanger (Harrison Radiator Company)

 

AF 5-40e (Industrial Engineers, Inc)

 

AF 5-40f (International Nickel Company) 1942-45

Physical Description: (1 folder)
 

AF 5-40g Preliminary Data

 

AF 5-40h Preliminary Data Solar Aircraft 1942-1945

 

AF 5-40i Preliminary Data. Trane Co. 1943-1945

Box Box 96

AF 5-45 Corres only re RMR A5B05. (1945).

 

AF 5-45 Corres only re RM ABE14. (1948).

 

AF 5-45 Corres only re RMR A5H23. (1947).

 

AF 5-45 Corres only re RMR TN 1312. (1947).

 

AF 5-45 P/D "Tests of Heat Exchange Design No. 35 Fabricated for AAF" by Kushnick March 15, 1943

 

AF 5-50 Exhaust Flame Suppression. October 16, 1942-March 29, 1943.

 

AF 6-20 Franklin Institute. 21 Oct 44 - Nov 20, 1944

 

AF 7-20 BF Goodrich Company. Sept. 11, 1941-Ap 13, 45

 

AF 8-5 Hamilton Standards Propellers. August 13, 1940- October 8, 1947

 

AF 8-10 Heaters Combination. October 20, 1941- August 6, 1945

 

AF 8-15 Hanlon Wilson Co. October 31, 1942-July 25, 1945

 

AF 9-10 Instruments - Ice Research General. November 22, 1940- October 14, 1946

Box Box 97

AF 9-10a Air Speed Indicator. May 28, 1941-July 1, 1941

 

AF 9-10b Ice Indication (Instruments) June 14, 1941-November 3, 1944

 

AF 9-10b Instruments- Ice Indicating. 1950-1951

 

AF 9-10b Preliminary Data. April 26, 1943

 

AF 9-10c Instruments-Aerometeorograph

 

10d Stall Warning Device

 

10e Measurement of Pressure Pulsations in Exhaust Gas Stream

 

10f Instruments (Actuators). 1948-1952

 

AF 10-10 Jack and Heintz Inc. January 5, 1945-August 9, 1945

 

AF 12-10 Landing Light de-icing.

 

12-15 Lightening, General.

 

12-15a Lightening, (Lockheed 12-a) 1941-1946

 

12-15b Lightening, (XC-35 LMAL)

Physical Description: [1 folder]
Box Box 98

AF 12-20 Lockheed Air Corp. Blueprints. November 6, 1941- April 23, 1947

 

AF 13-5 Martin Co. Glenn L. 1940-1946

 

AF 13-10 Massachussets Inst. Tech.

Box Box 98

AF 13-15 Mount Washington Observatory [Icing Data] 1944-1945

 

AF 15-3 National Bureau of Standards

 

15-5 Northrop Aircraft, Inc.

 

15-10 Northwest Airlines

Physical Description: 1 folder
 

15-15 North American Aviation Inc. [suggestions on antiicing methods] 1941-1945

Box Box 99

AF 16-10 Operation Aircraft in Icing Condition. 1941-1946

 

AF 16-10 [As above 1948]

 

AF 17-10 Program - Ice Investigation. March 24, 1941- September 18, 1944.

 

AF 17-10 [As above] 1952-1954

 

AF 17-20 Propeller De-icing - General. 1940-1946

 

[As above 1949-1950]

 

AF 17-20 [As above 1947-1948]

Box Box 100

AF 17-20 Loose blueprints and correspondence [Propeller icing data] 1945-1946

 

AF 17-20 Propeller De-Icing - General. [1949-1950]

 

AF 17-20a Propeller - Electric de-icing of prop. 1941-1947

 

AF 17-20b Prob de-icing (Geer Studies) July 8, 1942-March 17, 1943

 

AF 17-20c Prop de-icing. MIT

 

AF 17-20d Nat. Research Council of Canada

 

AF 17-20e Shere. Kahn. [de-icing shoes for prop]

 

AF 17-20f Propeller de-Icing. Trans-Canada Airlines

 

AF 17-20f-i TWA

 

AF 17-20g U.S. Rubber

Box Box 101

AF 17-24 Corres. only re A6G31 (1946-1947)

 

AF 17-25 Propeller De-Icing Reports. April 1943-July 45.

 

AF 17-25 P/D I "Illus. of Ice Formation on Props & Engine Cowling Fits..." Selna. June 30, 1945

 

AF 17-25 P/D "A Flight Investigation on the Effects of Air Discharge Orifices at the Tips of a Curtiss Air-Heated on the Propeller Thrust"

 

AF 17-25 P/D "Tests of Electric Thermal De Icing Equipment for Propellers." Rodert and Scherrer. April 17, 1943

 

AF 17-25 Corres only re CMR "Tests of Thermal-Electric De-Icing---by R. Scherrer and Lewis Rodert. (1943)

 

AF 17-25 Corres only re A6D09. (1946-1947)

 

AF 17-25 Corres only re A5E16. (1945)

 

AF 19-5 RANCO Inc. 1943

 

AF 19-10 Reports - De Icing - General

Box Box 102

AF 19-10a Reports-Progress-Special Sub Com on De-Icing. 1941-1942

 

AF 19-106 Reports-Progress-Weekly. AAL Progress Reports. 1941-1946

Box Box 103

AF 19-106-1 Reports-Progress MK Reports on B-24, B-17.

 

AF 19-106-2 Reports-Progress RAE Quarterly Statements.

 

AF 19-106-3 Reports-Progress Monthly Report for M/C.

 

AF 19-10c Prelim. Exhaust-Heat Wing De-Icing 1941.

 

AF 10-10d AR R-51 Exhaust Heat Wing De-Icing June 1941.

 

AF 19-10e [Title as above. 1941.]

 

AF 19-10f ARR-S2 Exhaust-Heat Wing De-Icing. August 12, 1941

 

AF 19-10h RMR Prelim. Invest. Air Healed Wing. March 14, 1942

 

AF 19-10h Corres. only re RMR "Prelim Inv. & Design of an Air Healed Wing for Lockheed 12 A Airplane" by Rodert & Jackson (1942-1943)

Box Box 104

AF 19-10i ARR Anti-Ice Equipment. Empl. Heated Air. June 26, 1942

 

AF 19-10j ACR Ju88 Anti-Icing Equip.

 

AF 19-10k CMR Thermal Ice Prevention Equipment B-24D September 11, 1942-January 28, 1943.

 

AF 19-101 Corres. only re A7122. (1948).

 

AF 19-20 Research-Ice Prevention-General. 1940-1946.

 

AF 19-20 [As above. 1944-1951]

Box Box 105

AF 19-20a Research-Exhaust gas-air mixture (RAN-1) August 31, 1944- May 23, 1947 [ice prevention]

 

AF 20-5 Specifications [De-Icing Systems] June 28, 1944-5 November 1946

 

AF 20-10 Stewart Warner Corp. September 1944-June 1947 [deicing]

 

AF 20-10 [Loose blueprints, drawings, correspondence Stewart Warner Corporation, AAL, NACA 1941-1944]

Box Box 106

AF 20-10 Preliminary Data Reports. Tests of Heat Excharger Designs and Carbon Monoxide Indicator. 16 February 1943-30 July 1943.

Physical Description: [4 folders]
 

AF 20-10 [Loose blurprints 1942]

 

AF 20-20 Suggested Studies-Ice Research. (1941-1945)

Box Box-107

AF 21-5 Tail Surface De-Icing (General) and AF 21-10 Temperature Measurements 1940-1944

Physical Description: [one folder]
 

AF 21-20 Terminology

 

21-30 Tests, De-Icing (General)

 

21-30a Tests conducted at LMAL

 

21-30f Tests, Participation-Discussion with Air Cos. 1941-1947

 

21-35 Trans Canada Air Lines

 

21-40 Trans Continental Western Air Lines, Inc.

Physical Description: [1 folder.]
 

AF 22-10 United Air Lines

 

22-15 US Rubber Co.

 

22-20 Calibration of Stainless - Steel Venturi Meter and U.C. 9 heat Meter 1941-1945

 

De-Icing information

Physical Description: [1 folder]
 

AF 22-20 University of California Research Program 1942-1945

Physical Description: [2 folders]
Box Box 108

AF 23-10 Vega Aircraft Company. 1943

 

AF 24-10 Weather Data. (1947-1948)

 

AF 24-10 Weather Data. 1943-57

 

AF 24-15 Corres re Weather Data. (1947-1948)

Physical Description: Reports.
 

AF 24-15 Corres re TN 1424. (1947-1948).

 

AF 15 Corres re TN 1387. (1947).

 

AF 15 Corres re TN 1393. (1948).

 

AF 15 Corres re TN 1434. (1948).

 

AF 15 Corres re TN 1472. (1947-1948).

 

AF 15 Corres re TN Gen Results of Flt Res - during Winter 1945-1946 TN (1947).

 

AF 24-15 Corres re ARR No 5613. (1945).

Box Box 109

AF 24-20 Windshield De-Icing. [1943 and 1948]

 

AF 24-20a Windshield De-Icing Aerotorque Company. [1940-1944]

 

AF 24-20a [Loose drawings, Blueprints. Windshield Assemblys. 1940]

 

AF 24-20b Windshield De-Icing American Air Lines

 

AF 24-20c Windshield De-Icing Repellant Lacquer

 

AF 24-20c Windshield De-Icing Rain Repellant Lacquer [1942-1948]

 

[As above. 1949]

 

AF 24-20d. [As above. Geer Frost Shield]

 

AF 24-20e. Patterson De-Icing System. [1943].

 

AF 24-25 Windshield De-Icing Reports, General. 1940-1942

Box Box 110

AF 24-25 P.D. "A Flt. Inv. in Natural Icing Condition of a Heated-Air External Discharge System for Wind-Shield Ice Prevention" by Holdaway. 6/20/46.

 

AF 24-25 P.D. "Investigation of Eff. of Two Types of Alcohol on Windshield of XB-24F." Rodert and Neel. April 12, 1943.

 

AF 24-25 Corres only re A5E25. (1947)

 

AF 24-25 Corres only re A6I30. (1947)

 

AF 24-25 Corres only re A5:21. (1946)

 

AF 24-30 Wing De-Icing - General. 1949-1950

 

AF -30a Wing De-Icing - Navy. (PBY). [1941-1944]

 

AF -35 Corres only re TN 1675. (1948)

 

AF 24-65 Tests. 1955.

Box Box 111

AM 1-5 Accidents. [1943-1945]

 

AM 1-10 Airsearch Manufacturing. [1942-1943]

 

AM 1-20a Airplanes - B-24. [1943-1944]

 

AM 1-20b Airplanes - B-17. [1943-1944]

 

AM 1-20c Airplanes - C-46 [1943-1945]

 

AM 1-20d Airplanes - Lockheed 12-A. [1943]

 

AM 1-20e Airplanes - XC-53. [1943]

 

AM 1-20f Airplanes - P-42. [1942]

 

AM 1-20g Airplanes - XC-60B. [1943-1944]

 

AM 1-20h Airplanes - B-26. [1942-1943]

 

AM -20i Airplanes - Wellington Bomber. [1943]

 

AM -20j Airplanes - B-25. [1942-1943]

 

AM -25 American Airplanes. [1942-1943]

 

AM -27 Antennae De-Icing - Radio, Radar. [1943]

 

AM -30 Army Air Forces - Material Command. [1943-1944]

 

AM -30a Army Air Forces - ADTIC. [1943]

Box Box 112

AM 2-10 Bendex Aviation Corporation. [1941-1943]

 

AM -30 British Air Commission. [1942-1944]

 

AM 3-15 Compounds and Solutions - De-Icing. [1942-1945]

 

3-10 Cars-Storage, Gas, Etc. [1943]

 

AM 3-30 Correspondence - General. [1942-1944]

 

AM 3-30 Curtiss-Wright Corporation - General. [1945]

 

AM -30a Curtiss-Wright Corporation - Propeller Division [1942-1945]

 

AM 5-20 Engine Research Laboratory. [1943-1945]

 

AM 7-10 Geer Frost Shields. [1943]

 

AM -15 General Electric Company. [1942]

 

AM -20 Goodrich, B.F., Company. [1943-1944]

 

AM 8-10 Hamilton Standard Propellers. [1942-1943]

 

AM 8-15 Harlon and Wilson Company. [1943]

 

AM 8-20 Hartman, E. P. [1943]

 

AM 9-10 Ice Rsearch Projects - Genreal Correspondence [1944]

 

AM 9-10a Ice Research Projects - Tests in Vicinity of Seattle. March 1941

 

AM 9-10b Ice Research Projects. Tests in Vincinity of Minneapolis. April 1944.

 

AM 9-10c Ice Research Projects. Tests in Vincinity of Minneapolis. Nov-Dec. 1941

 

AM 910e Ice Research Projects. Tests in Vincinity of Minneapolis. 1944-1945

 

AM 9-12 Induction System De-Icing. [1942-1945]

 

AM 9-15 IRB Offices - Regulations, Equipment, Etc. 1942

 

AM 9-20 Instruments - General. [1943-1944]

 

AM -20a Instruments - On Loan to IRP. [1943-1944]

 

AM -20b Instruments - Ice Indicating. [1943-1945]

 

AM -30 Inventory. [N.D.C. 1943]

 

AM 12-5 Ladd Field Operations. [1942-1943]

 

AM 14-5 McQuay, Incorporated. [1943-1944]

Box Box 113

AM 14-10 Martin, Glenn L., Company. [1943]

 

AM -15 Massachusettes Institute of Technology. [1942-1943]

 

AM 14-20 Meetings - General. [1945]

 

AM -20a Meetings - SAE Sub-Committee. [1943-1944]

 

AM 14-20b Meetings - Sub-Committee on De-Icing. [1943-1944]

 

AM 15-10 NACA-Washington - General Correspondence. [1942-1943]

 

AM 15-15 National Defence Research Committee. [1943]

 

AM -20 National Research Council of Canada. [1942-1943]

Physical Description: [CLOSED]
 

AM 15-25 Navy Department-Bureau of Aeronautics. [1942]

 

AM 15-30 Northwest Airlines Incorporation. [1942-1945]

 

AM 16-10a Olsen, Major A.E. - Progress Reports [1942-1945]

 

AM 16-15 Organization - General - 1942-1943

 

AM -15a Organization - General - 1943-1944

 

AM -15b Organization - General 1944-1945

 

AM 17-5 Photographs - Films, etc. [1943]

 

AM -10 Pilots. [1943]

 

AM -14 Pilot Static Tube Investigation. [1943]

 

AM -15 Pittsburgh Plato Glass Company. [1943]

Box Box 113

AM 17-20 Pratt & Whitney Aircraft. [1943]

 

AM -25 Precipitation Static Research. [1942-1943]

Box Box 114

AM -30 Propeller De-Icing. [1943-1945]

 

AM 17-35 Program - Research. [1943-1944]

 

AM 19-10 Research - General. [1942-1945]

 

AM -15 Reports - General. [1942-1945]

 

AM -20 Rodert, Lewis A. - General. [1942-1944]

 

AM -20a Rodert, Lewis A. - General Letters to S. J. DeFrance 1942-1944

 

AM 20-15 Standard Alcohol Company. [1942-1945]

 

AM 20-20 Stewart-Warner Corporation. [1942-1945]

 

AM 21-5 Tests - General. [1942]

Box Box 115

AM 21-5a Tests - Progress Reports. [1942-1945]

 

AM 21-5b Tests - B-24 Engine Nacelle Ground Test. [1942]

 

AM 21-5c Tests - Blimp De-Icing Tests. [1944-1945]

 

AM -10 Trane Company. [1943-1944]

 

AM 21-15 Trms-Canada Air Lines. [1942]

 

AM 21-20 Transcontinental and Western Air, Inc. [1942-1943]

 

AM -25 Travel. [1944-1945]

 

AM 22-10 United Air Lines. [1943-1944]

 

AM -13 United Aircraft Corporation. [1942]

 

AM -15 United States Rubber Company. [1943]

 

AM -20 University of California. [1942]

 

AM 23-10 Vega Aircraft Corporation. [1943]

 

AM -15 Visits and Visitors - General. [1942-1945]

 

AM 24-10 Weather Bureau - General. [1943-1944]

 

AM 24-10a Weather Bureau - Weather Reports. [1943-1944]

 

AM 24-15a Windshield De-Icing. [1943]

 

AM -15a Windshield De-Icing. Bird Impact Tests. [1942]

Box Box 116

AR 1-5 Aberdeen Proving Grounds. [1944-1946.

Physical Description: 2 folders]
 

AR 1-5 Accidents - Ames [1944]

 

AR 1-5 Accidents October 14, 1944-March 31, 1947. [Reports and Ames regarding air crashes during tests. Included in the reports are a discription of the cause, the accident, some explanation for the accident, photographs of the equipment, and testimony regarding the accidents.]

Box Box 117

AR 1-5 Accidents - Airplane. 1941-1947

Box Box 118

AR 1-5 Accidents - Airplane. 1948

Box Box 119

AR 1-10 Aircraft Movement - SAL 1941-1951

 

AR 1-12 Airfields. (1947-1948)

 

AR 1-14 Airplanes - General. 1942-1949

 

AR 1-14 Airplanes - Estimates of Air Force Airplanes Desired at Ames, July 1942 to Nov. 1951

 

AR 1-15a Airplanes F2A-3 Brewster.

Scope and Content Note

Test data [changes etc. requistions, especially accident reports.]
 

AR 1-15a-1 Airplane Calibration F6F-3. 1945

 

AR 1-15a-2 Airplane Calibration XBT2D-1. 1945-1948

Box Box 120

AR 1-15a-3 Airplanes. F404. 1945-1946

 

AR 1-15a-4 Airplanes. P-80A (R.A.A. - 183). (1946-1948)

 

AR 1-15a-5 Dynamic Stability and Control of Airplanes. (RA A-181) (1947)

 

AR 1-15a-9 Flight Operations. Aug. 1944-June 1948.

 

AR 1-15b Airplanes - OS20-2. [1951]

Box Box 121

AR 1-15b Airplanes. 1942-1944. [Navy OS20-2. research memos, Naval specification bulletins, requisitions, accident report.]

 

AR 1-15c Airplanes. F24 1941-45. [Accident report, bill of lading, Commos between NACA & Mfg.]

 

AR 1-15d Airplanes F4F [As w/15b.]

 

AR 1-15e Airplanes P38. [1943-45. as above]

 

No Code YP-80 A. 1946

Physical Description: [blueprints]
 

AR 1-15f Airplanes C-46. 1943-44 [Requisitions, shipping notices, info on bulge controls, blueprints.]

Box Box 122

AR 1-15g Airplanes A20-A 1939-1943

Scope and Content Note

[Correspondence, drawings, blueprints, photos re. equipment specifications & characteristics.]
 

AR 1-15h Airplanes B-25D. 1941-1943

Scope and Content Note

[as above]
 

AR 1-15i Airplanes P-39 N 1943-1944

Physical Description: [2 folders]

Scope and Content Note

[as above] AR1-15i PD to above - 1943.
 

AR 1-15j Airplanes a-35. 1943 [as above]

 

AR 1-15k Airplanes A25 1943 [re testing]

Box Box 123

AR 1-151 Airplanes P51 1943-47 [as with A20a]

 

AR 1-15m B-26 B 1943-1947 [as above]

 

AR 1-15n Airplanes SB2C-1. 1943 [re testing]

 

AR 1-15n PV-1 (Lockheed) 1944-45. [Flight test reports, modifications, blueprints]

 

AR 1-15p Airplanes P-61A [Shipping tickets, receipts, memos on testing, specifications]

 

AR 1-15q Airplanes VTD-1 1944-45 [Correspondence, blueprints as above.]

Box Box 124

AR 1-15r Airplanes XP56. July 44

Physical Description: [One Memo]
 

AR 1-15s Airplanes XF7F-1. 1945 [As with 15p]

 

AR 1-15t XBT 20-1. Airplane - [1946]

Physical Description: 2 folders.
 

AR 1-15t Airplanes

 

(AR 1-15u) P-75 General Motors

 

AR 1-15v Airplanes YP-80. July 1944-Feb. 1948

 

AR 1-15w Airplanes P-47

Box Box 125

AR 1-15x Airplanes FR-1. 1945-46

 

AR 1-15y Airplanes FN-2. 1945

Physical Description: [Invoices, telegrams re procurement & disposale of the above for test purposes.]
 

AR 1-15z Airplanes F6F-3. 1945. [as above w/drawings]

Box Box 126

AR 1-15-1 XS-3 (Douglas). [1948]

 

AR 1-15-2 XS-4 (Douglas). (MX-810) [1949]

 

AR 1-15-4 D-558-I & D-558-II (Douglas) 1947 thru Oct. 1948.

 

AR 1-15-4 D-558-I & D-558-II (Douglas) Nov. 1948-1949

Box Box 127

AR 2-10

 

AR 3-10 [Carbon Monoxide Indicators. 1945-1948]

 

AR 5-5 Engines. [1946-1948]

 

AR 6-10 Flight Regulations. [1943-1945]

 

AR 8-10 High Altitude Flying. [1942-1948]

 

AR 2-10 Booster Units. (1947-1948)

 

AR 9-5 Instrument Ratings - Pilots. (1942-1945)

 

AR 9-10 Instruments 1940-1946 [Re instruments needed or ulitized at Ames. Also requests for equip.]

Box Box 128

AR 9-10a-10f Instruments. 1943-47 [as above w/photos, blueprints, reports, etc.

Physical Description: (3 folders)]
 

AR 9-15 Insurance - Flight. 1944-45.

Physical Description: [Memos & application forms]
 

AR 12-10 Link Trainer Instruction. 1942

Physical Description: [Memos & letters]
 

AR 17-10 Pilots - Test. [1941-1949]

 

AR 17-17 Pressure Suits. [1943]

 

AR 17-20 Propeller, Balancing Equipment, General Correspondence

 

AR 17-25 Propellers-General. [1944-1948]

Box Box 129

AR 17-25a Propellers-Reserve Pitch. 1947

 

AR 19-5 Radio-General. [1947]

 

AR 19-5a Radio Controlled Models. 1941-1946

Physical Description: [2 folders]
 

AR 19-5a Radio Controlled Models. (1947)

 

AR 19-6 Radio - Range Trainer. [1949]

 

AR 19-8 Radar 1944-1945

 

AR 19-8 Radar - 1947

 

AR 19-10 Reports - General 1943-1945

Box Box 130

AR 19-10a-8 RA A199. Drawings - F-86. 1947

 

AR 19-10a-8 RA A199. Drawings. XF-86. 1948

Box Box 131

AR 19-10b Reports OSU-2. 1945

Physical Description: [Gen. Cor. & Blueprints]
 

AR 19-10b PD Reports. April 26, 1945-July 24, 1945

 

AR 19-10c Reports F2A3. July 25, 1942 [contains PD Report]

 

AR 19-10e Reports - B-24D. [Contains Gen Cor & PD Report dtd. April 8, 1943]

 

AR 19-10f Reports B17f. [GC & PD dated April 27, 1943]

 

AR 19-10g Log Reports. P-38F.

Scope and Content Note

[As above. PD dated June 11, 1943]
Box Box 132

AR 19-10h Reports C46. May 3, 1944-October 9, 1944

 

AR 19-10i Reports. B25D. January 29, 1944 - June 22, 1945

 

AR 19-10j Reports A20A. 30 June 43

 

AR 19-10k Reports P-39N-1. January 3, 1944-28 June 1946

 

AR 19-10m Reports P51-B. June 1, 1944

Box Box 133

AR 19-10p Reports P61-A.

 

10p Reports FR-1.

Box Box 134

AR 19-10r Reports FR-1.

 

AR 19-10q Reports YP-4FM-1; P-47N-1.

Box Box 135

AR 19-10r Reports FR-1.

 

AR 19-10s Reports P75A-1.

 

AR 19-10t Reports. XBT2 0-1.

Box Box 136

AR 19-10v Reports YP-80a.

Box Box 137

AR 19-10w Reports A 26 B.

 

AR 19-10z Reports P-80a.

 

AR 19-15 Research - Flight - General.

 

AR 19-15 Research-Flight-General. (1947-1948).

Box Box 138

AR 19-15a - AR 19-15d. Research. 1943-1945. [Reports, flight studies and minutes of conferences held by NACA officials with USAAF and Navy Personnel regarding fighter specifications and problems in fighter design.]

Physical Description: (3 folders)
 

AR 19-15d Research - Specification "Stability & Control Char." [1947-50]

 

AR 19-25 Research Problems Suggested. [1940-1950]

Box Box 139

AR 20-5 Scales-Aircraft. July 1943 - 31 July 194

 

AR 20-10a Supplies & Equip.-General. 1942-45

 

AR 20-10 Supplies & Equipment-General (1947-48)

 

AR 20-10b Supplies & Equip-Langley. 1941-1943

 

AR 21-5 Tests-General. (1943-1945)

 

AR 21-5a Tests-Progress Reports. Flight Research July 18, 42-Feb. 5, 46

Scope and Content Note

[Wind Tunnel schedules and aircraft utilized; problems worked on, etc.]
 

AR 21-5b Tests-Progress Reports. Flight Operations [Section] May 1, 1943-October 26, 1944

 

AR 21-5c Priority of tests (1947-1948).

Box Box 140

AR 21-5c [Subjects: Test Priorities, schedules, weight and center of gravity, dynamic lift of airships, and correlation of wind tunnel and flight tests.]

 

AR 21-59 MARS PB2M Flying Boat. June 23, 1944-July 1, 1944

Box Box 141

AT 1-10 Accidents. Theoretical and Applied Research Division. March 27, 1942 - December 9, 1947.

Scope and Content Note

Accident reports and comments exchanged between Langley, Cleveland, and Ames, mostly about accidents in wind tunnels. Reports include a description of the cause, the accident, some explanation for the accident, and often photographs of the equipment and/or testimony regarding the accident.
 

AT 1-10 Accidents-General. 1943-1948

Box Box 142

AT 2-5 Balancing Equipment - General. Theoretical and Applied Research Division. July 30, 1946 - September 21, 1940.

 

AT 2-5a Balancing Equipment - Hinge Movement. August 29, 1941 and August 25, 1941.

Scope and Content Note

[Includes drawing and data for hinge-movement balance.]
 

AT 3-10 Couplings. October 20, 1941 - June 9, 1941.

Scope and Content Note

[Dynamic Corporation, G.E., and others].
 

AT 4-20 Design-Wing Tunnel. 1948

 

AT 4-20 Design-Wind Tunnels - General. October 12, 1943 - December 10, 1940. December 5, 1947 -

Physical Description: [Folder 1]
Box Box 143

AT 4-20 Design - Wind Tunnels - General. October 12, 1943 - December 10, 1940. December 5, 1947 -

Physical Description: [Folders 2 and 3]

Scope and Content Note

Some good photographs and descriptions of the facilities.]
 

AT 4-50 Dynamometer Equipment. August 1944 - March 18, 1941.

Scope and Content Note

[Operational instructions, parts lists, etc. from various contractors.]
 

AT 5-10 Engine Research Laboratory - General Design. March 31, 1944 - 1940.

Box Box 144

AT 5-10a Engine Research Laboratory - Material and Equipment. April 29, 1947 - 1941.

 

AT 5-10b Engine Research Laboratory - Power Supply. 1941-1948.

 

AT 5-10c Engine Research Laboratory - Progress Reports - Design. 1944.

 

AT 5-10d Engine Research Laboratory - Propellors. 1941-1943.

 

AT 5-10e Engine Research Laboratory - Icing Research. 1943/

 

AT 5-20 Equipment, General. December 1947 - February 1942.

 

AT 5-20 Equipment - General. (1946-1948)

 

AT 5-20 Equipment, General. (1948)

Box Box 145

AT 5-20 Equipment, General

 

AT 5-20 Equipment, General

Box Box 146

AT 5-20a Equipment, - Strain (Guage) Equipment. (1948).

 

AT 5-20a Equipment - Strain Gage. August 8, 1941 - December 1947.

Box Box 147

AT 5-20b Equipment - Tachometer

 

AT 5-20c Equipment - Ear Wardens

 

AT 5-20d Equipment - Interferometer. (1945-1948/

 

AT 14-20 Models - General

Box Box 148

AT 14-20 General 1948-1949. Also AT 14-20 Models. Conical Shock Differers. 1949

Box Box 149

AT 14-20a Models - Specifications

 

AT 14-20a Models - Specifications 1948

Box Box 150

AT 14-20b Models - Supports

Box Box 151

AT 14-20b Models - Supports

Box Box 152

AT 14-30 Motors - General

 

Full-Scale Tunnel Power Equipment, Westinghouse

 

Full-Scale Tunnel Power Equipment, G.E.

 

AT 14-30a Motors - Generator Equipment

 

AT 14-30b Motors - Model

Physical Description: (2 folders)
Box Box 153

AT 14-30c Motors - Self Synchronizing

 

AT 17-20 Propellors - General

Physical Description: [2 folders]
Box Box 154

AT 17-20 Drawings. [Supersonic Propeller) 1951.

 

Drawings.

Physical Description: [2 folders]
Box Box 155

AT 19-5 Rake Tube April 16 - July 14, 1945.

 

AT 19-10 Refrigeration

 

AT 19-20 Research - General March 25, 1941 - April 30, 1947

 

AT 21-15 Television. (1948)

 

AT 21-20 Tests - General July 23, 1941 - October 3, 1947

 

AT 21-40a Tunnels - General. Preliminary Design. 1942.

 

(AT-1) 4-20 Drawings - General Re 7 x 10 tunnel

 

(AT-1) 5-20 Equipment - General Re 7 x 10 tunnel

Box Box 156

(AT-1) 5-20a Equipment - Survey Apparatus

 

(AT-1) 16-20 Operations - General

 

(AT-1) 17-20 Program Research

 

(AT-1) 19-15 Research Problems XP-5Y-1

 

(AT-1) 21-5 Tests - General

 

(AT-1) 21-5b Tests - Progress Reports. September 20, 1941-February 5, 1946.

Physical Description: [2 folders]
 

(AT-1) 21-5c Tests - Turbulence level

Box Box 157

(AT-1) 21-10 Tests XB-32

 

(AT-1) 21-10a Tests. Preliminary Results

Scope and Content Note

Preliminary Data on Force Test Characteristics of the XB-32 Flapped Wing. Myles D. Erickson. July 9, 1942. Preliminary Data From 7-by 10-foot Wind Tunnel Tests on the XB-32 Flapped Wing. M.D. Erickson. June 29, 1942
Box Box 158

(AT-1) 21-20 Tests XSB2D-1

 

(AT-1) 21-20a Preliminary Results

 

(AT-1) 21-20a Correspondence

Box Box 159

(AT-1) 21-20a Preliminary Results

Box Box 160

(AT-1) 21-20a Preliminary Results

Box Box 161

(AT-1) 21-20a Preliminary Results

Box Box 162

(AT-1) 21-20a Preliminary data reports, 1942-1943.

Box Box 163

(AT-1) 21-20a Preliminary data reports, 1943.

Box Box 164

(AT-1) 21-20a Preliminary data reports, 1942 and 1944.

Box Box 165

(AT-1) 21-20a Preliminary data reports, 1942.

Box Box 166

(AT-1) 21-20a Preliminary data reports and loose blueprints, 1942.

Box Box 167

(AT-1) 21-20a Loose blueprints and reports, 1942.

Box Box 168

(AT-1) 21-25 Tests D-2. Hughes. 1941-1942.

 

AT-1 21-25 CMR Tests on Hugher D-2 in 7 x 10 - 1942-1944

 

(AT-1) 21-30 Tests XB-28. 1942.

Box Box 169

(AT-1) 21-30a Preliminary Results, 1941-1942.

 

(AT-1) 21-30b Tests XB-28 1941-1942.

 

(AT-1) 21-30b Tests. XB. 24" Const. Chord Wing

 

(AT-1) 21-40 Tests XB-35. Northrop Aircraft. 1942-1943.

 

(AT-1) 21-45 Tests Ailerons. 1942.

Box Box 170

(AT-1) 21-45 Prob. TR "WT Inv of the Effects of Profile Mod. and Tabs on the Charac. of Aikrons on a low-drag Airfoil" by Crane and Holtzclaw. [1947]

Box Box 171

(AT-1) 21-50 Tests. XPB3Y-1. Consolidated. 1942-1943.

Box Box 172

(AT-1) 21-50a Preliminary Results. 1942.

 

(AT-1) 21-55 C-47 Drawings

 

(AT-1) 21-55 Tests. C-47. Douglas. 1942; 1944.

Box Box 173

(AT-1) 21-55a Preliminary Results. 1942-1945.

 

(AT-1) 21-60 Tests. XPV-2. Vega.

Physical Description: [drawings]
Box Box 174

(AT-1) 21-60 Tests. XPV-2. Vega. 1942-1943.

 

(AT-1) 21-60a Preliminary Results. 1943.

Box Box 175

(AT-1) 21-65 Tests. XCG-13. Glider, Waco. 1943-1944.

 

(AT-1) 21-65a Tests XCG-13. Preliminary Results. 1943.

 

(AT-1) 21-70a Tests. PBY-5B. Preliminary Results. 1943.

 

(AT-1) 21-75a Tests. PV-1. Preliminary Results.

Box Box 176

(AT-1) 21-75a Tests. PV-1. 1943

 

(AT-1) 21-75 Tests. PV-1. 1943.

 

(AT-1) 21-80 Tests. XA-39. Fleetwings. 1943.

Physical Description: [drawings]
Box Box 177

(AT-1) 21-80 Tests. XA-39. Fleetwings. 1943.

Physical Description: [drawings]
Box Box 178

(AT-1 21-80 Tests. XA-39. Fleetwings. 1943.

Physical Description: [drawings and reports]
Box Box 179

(AT-1) 21-80a Preliminary Results. 1943.

 

(AT-1) 21-85 Tests. XFR-1. 1944-1945.

Box Box 180

(AT-1) 21-85 Tests. XFR-1. 1943.

Box Box 181

(AT-1) 21-85 Tests. XFR-1.

Physical Description: [drawings]
Box Box 182

(AT-1) 21-85 Tests. XFR-1.

Physical Description: [drawings]
 

(AT-1) 21-85a Preliminary Results. 1943-1946.

Box Box 183

(AT-1) 21-85a Preliminary Reports. 1943.

Box Box 184

(AT-1) 21-85a Preliminary Reports. 1944-1945.

Box Box 185

(AT-1) 21-85a Preliminary Reports. 1945.

Box Box 186

(AT-1) 21-100 Tests. XP2V-1. Vega. 1943-1945.

Physical Description: [drawings]
Box Box 187

(AT-1) 21-100a Preliminary Results. 1943.

Box Box 188

(AT-1) 21-100a Preliminary Results. 1944.

Box Box 189

(AT-1) 21-100a Preliminary Results. 1943-1944.

Physical Description: [drawings]
 

(AT-1) 21-105 Tests. C-74. Douglas. 1943.

Box Box 190

(AT-1) 21-105a Preliminary Results. 1943-1944.

 

(AT-1) 21-110 Tests. XB-36. Consolidated. 1943-1944.

Box Box 191

(AT-1) 21-110 Tests. XB-36. Consolidated.

Physical Description: [drawings and contractor reports]
 

(AT-1) 21-110a Preliminary Results. 1943-1945.

Box Box 192

(AT-1) 21-110a Preliminary Results. 1943-1944.

Box Box 193

(AT-1) 21-110a Preliminary Results. 1944-1945.

 

(AT-1) 21-115 Tests. XTB2D-1. Douglas. 1943.

Box Box 194

(AT-1) 21-120 Tests. XA-41. Consolidated. 1943-1944.

 

(AT-1) 21-120a Preliminary Results. 1943-1944.

 

(AT-1) 21-125 Tests. XFD-1. McDonnell. 1943-1945.

Box Box 195

(AT-1) 21-125 Tests. XGD-1. McDonnell.

Physical Description: [drawings]
Box Box 196

(AT-1) 21-125a Preliminary Results. 1943-1945.

Box Box 197

(AT-1) 21-130 Tests. XBDR-1. 1943-1944.

Physical Description: [drawings and correspondence]
Box Box 198

(AT-1) 21-130 Tests. SBDR-1.

Physical Description: [drawings]
Box Box 199

(AT-1) 21-135 Tests. XBDR-1 Flow Model Interstate. 1944.

 

(AT-1) 21-135a Interstate Preliminary Results.

Box Box 200

(AT-1) 21-140 Tests. XB-42. Douglas. 1943-1944.

 

(AT-1) 21-140a Preliminary Results. 1943-1945.

Box Box 201

(AT-1) 21-140a Preliminary Results.

Box Box 202

(AT-1) 21-145 Tests. TED-2323. Consolidated Vultee. 1944.

Physical Description: [drawings]
Box Box 203

(AT-1) 21-145 Tests. TED-2323. Consolidated Vultee.

Physical Description: [drawings]
 

(AT-1) 21-145a Preliminary Results. 1944.

 

(AT-1) 21-150 and 21-150a Tests. F-11. 1944-1945.

 

(AT-1) 21-152 Tests. XP-79. Avion. 1944

Box Box 204

(AT-1) 21-152 Tests. XP-79.

Physical Description: Photos and drawings.
Box Box 205

(AT-1) 21-152 Tests. XP-79

Physical Description: [drawings and photos]
 

(AT-1) 21-152a Preliminary Results. 1944.

 

(AT-1) 21-155 Tests. BTD-1. Douglas. 1944.

Box Box 206

(AT-1) 21-155a Preliminary Results.

Physical Description: [drawings]
 

(AT-1) 21-20 Tests. XSB2D-1. [see also box 15]

 

(AT-1) 21-155a BTD-1. Preliminary Results. 1944.

Box Box 207

(AT-1) 21-157 Tests. XP-81. Consolidated. 1944.

Physical Description: [drawings]
Box Box 208

(AT-1) 21-157 Tests. XP-81. Consolidated

Physical Description: [drawings]
 

(AT-1) 21-157a Preliminary Results. 1944

Box Box 209

(AT-1) 21-157a Preliminary Results. 1944.

 

(AT-1) 21-160 Tests. VT2D-1. Douglas. 1944-1945.

Physical Description: [drawings]
Box Box 210

(AT-1) 21-160 Tests. BT2D-1. Douglas.

Physical Description: [drawings]
Box Box 211

(AT-1) 21-160a Preliminary Results. 1944.

Box Box 212

(AT-1) 21-160a Preliminary Results. 1944-1945.

Box Box 213

(AT-1) 21-162a Tests. NDRC. Douglas missile. Preliminary Results.

Box Box 214

(AT-1) 21-162a Preliminary Results.

Box Box 215

(AT-1) 21-165 Tests. XF15C-1. Curtiss.

 

(AT-1) 21-165a Preliminary Results. 1945.

Box Box 216

(AT-1) 21-165a Preliminary Results. 1944-1946.

Box Box 217

(AT-1) 21-165a Preliminary Results. 1944-1946.

 

(AT-1) 21-170 Tests. XF15C-1. Curtiss Wright. Duct Entries. 1944.

Box Box 218

(AT-1) 21-170 Tests. XF15C-1. Curtiss Wright.

Physical Description: [drawings]
Box Box 219

(AT-1) 21-170 Tests. XF15C-1. Curtiss Wright.

Physical Description: [drawings]
 

(AT-1) 21-170a Preliminary Results. 1944-1945.

Box Box 220

(AT-1) 21-170a Preliminary Results. 1944.

 

(AT-1) 21-175 Tests. F-11 Hughes. 1944-1945.

Physical Description: (60-inch span model)
Box Box 221

(AT-1) 21-175 Tests. F-11. Hughes.

Physical Description: [loose drawings]
 

(AT-1) 21-175a Preliminary Results. 1944-1945.

Box Box 222

(AT-1) 21-175a Preliminary Results. 1944-1945.

 

(AT-1) 21-180 Duct Entrances. [re submerged-type inlets for engine charge air] 1945

 

(AT-1) 21-180a Preliminary Results. 1945.

Box Box 223

(AT-1) 21-182 Tests. XP-81 Airfoil Section. 1945

 

(AT-1) 21-182a Preliminary Results. 1944-1945.

Box Box 224

(AT-1) 21-185 Tests. XB-35 Propeller Tests. Northrop A-151. 1943-1945.

Box Box 225

(AT-1) 21-185 Tests. XB-35 Propeller Tests. Northrop A-151.

Physical Description: [drawings]
Box Box 226

(AT-1) 21-185 Tests. XB-35 Propeller Tests. Northrop A-151.

Physical Description: [drawings]
 

(AT-1) 21-185a Preliminary Results. 1945.

 

(AT-1) 21-190 Tests. XB-46. Consolidated. 1944-1945.

Box Box 227

(AT-1) 21-190a Preliminary Results. 1944-1946.

Box Box 228

(AT-1) 21-195 Tests. XB-46. Horizontal Tail Model. 1945.

 

(AT-1) 21-195a Preliminary Results. 1945-1947.

Box Box 229

(AT-1) 21-205 Tests. XP-81. 1945.

 

(AT-1) 21-205a Preliminary Rssults. 1945.

 

(AT-1) 21-215 Tests. XF15C-1. 1945

 

(AT-1) 21-215a Preliminary Results. 1945.

Box Box 230

(AT-1) 21-215a Preliminary Results. 1945.

 

(AT-1) 21-220 Tests. XF2R-1. Inv. of cowling and exit duct pressures, propeller cuffs, and stability of

 

(AT-1) 21-220a Preliminary Results.

Box Box 231

(AT-1) 21-245 Tests. XF2R-2 Airplane, Ryan. 1946.

Box Box 232

(AT-1) 21-245 Tests. XF2R-2 Airplane. Ryan.

Physical Description: [drawings]
Box Box 233

(AT-1) 21-245a Preliminary Results.

 

(AT-1) 21-250 Tests. CV model 240. 1946.

Box Box 234

(AT-1) 21-250 Tests. CV model 240. 1946.

Physical Description: [drawings]
 

(AT-1) 21-260. Tests. Conventional and Vee Tail Arrangements. (A-127) 1947

Box Box 235

(AT-2) 3-15 Communication System. 1942-1945.

 

(At-2) 3-20 Design Data. 1942-1945.

 

(AT-2) 5-20 Equipment, General. [1941-1950 re]

Physical Description: 16 ft. wind tunnel
 

(AT-2) 5-20 Equipment, General. (1942-1947)

Physical Description: [2 folders]
 

(AT-2) 5-20 Equipment, Survey Apparatus (1946-1947)

Box Box 236

(AT-2) 16-20 Operations, General. [(1942-1945 re 16 ft. wind tunnel]

 

(AT-2) 14-10 Medical Certificate-Manufactures Repr. (1942-47)

 

(AT-2) 17-10 Personnel, physical examination. 1942-1946.

 

(AT-2) 17-20 Program Research. 1942-1947.

Physical Description: (16. ft. wind tunnel)
Box Box 237

(AT-2) 19-15 Research Problems and Suggestions. 1946-1942.

Physical Description: (16 ft. wind tunnel)
 

(AT-2) 21-5 Tests, General. 1942-1945. [reports and samples from camouflage tests in 16 ft. wind tunnel]

 

(AT-2) 21-5b Tests, Program Reports. 1942-1946. ["Progress reports and tunnel schedules" Monthly re 16 ft. wind tunnel]

Box Box 238

(AT-2) 21-10 Loose Blueprints. 1944.

Box Box 239

(AT-2) 21-10 Tests. XSB2D-1 Douglas. 1942-1948.

Box Box 240

(AT-2) 21-10 Tests. XSB2D-1. Douglas.

Physical Description: [drawings]
Box Box 241

(AT-2) 21-10 Tests. XSB2D-1. Douglas.

Physical Description: [drawings]
Box Box 242

(AT-2) 21-10 Tests. XSB2D-1. Douglas.

Physical Description: [drawings]
Box Box 243

(AT-2) 21-10 Tests. XSB2D-1. Douglas.

Physical Description: [drawings]
Box Box 244

(AT-2) 21-10 Tests. XSB2D-1. Douglas.

Physical Description: [drawings]
Box Box 245

(AT-2) 21-10a Preliminary Results. 1943-1947.

Box Box 246

(AT-2) 21-10a Preliminary Data. August 1943-November 19, 1943.

Box Box 247

(AT-2) 21-10a Preliminary Results. November 25, 1943-December 4, 1943.

Box Box 248

(AT-2) 21-10a Preliminary Results. December 6, 1943-December 14, 1943.

Box Box 249

(AT-2) 21-10a Preliminary Results. December 15, 1943-January 8, 1944.

Box Box 250

(AT-2) 21-10a Preliminary Results. January 11-28, 1944.

Box Box 251

(AT-2) 21-10a Preliminary Results. February - April 3, 1944.

Box Box 252

(AT-2) 21-10a Preliminary Results. April 4-18, 1944.

Box Box 253

(AT-2) 21-10a Preliminary Results. April 19, 1944 - September 1944.

Box Box 254

(AT-2) 21-10a Preliminary Results. October 1944 - July 1945.

Box Box 255

(AT-2) 21-10a Preliminary Results. November 1945.

Box Box 256

(AT-2) 21-10 Tests XB36. Consolidated. Mat. Div. 1942-1945.

Box Box 257

(AT-2) 21-10 Tests XB36. Consolidated. Mat. Div. 1942-1945.

Box Box 258

(AT-2) 21-10 Tests XB36. Consolidated. Mat. Div. 1942-1945.

Box Box 259

(AT-2) 21-10 Tests XB36. Consolidated. Mat. Div. 1942-1945.

Box Box 260

(AT-2) 21-10 Tests XB36. Consolidated. Mat. Div. 1942-1945.

Box Box 261

(AT-2) 21-10 Tests XB36. Consolidated. Mat. Div. 1942-1945.

Box Box 262

(AT-2) 21-10 Tests XB36. Consolidated. Mat. Div. 1942-1945.

Box Box 263

(AT-2) 21-20a Tests XB-36. Consolated Prelim Results. 1943-1944.

Box Box 264

(AT-2) 21-20a Tests XB Consolated Prelim Results. 1943-1944.

Box Box 265

(AT-2) 21-25 Tests XP-54. Ducting System Mat. Div.

Box Box 266

(AT-2) 21-25 Blueprints. 1942.

Box Box 267

(AT-2) 21-25a Tests XP-54. Ducting System. Mat. Div. Prelim Results. 1944

 

(AT-2) 21-25a Tests XP-54. Preliminary Results.

Physical Description: [3 folders]
Box Box 268

(AT-2) 21-30 Tests. XP-54. Lockheed. 1944

Box Box 269

(AT-2) 21-30a Tests. XP-38. Lockheed. Preliminary Results.

 

(AT-2) 21-30a Preliminary Data from 16 foot Wind-Tunnel Tests of the Lockheed P-38 Model. Albert D. Erickson. May 20, 1942.

 

(AT-2) 21-30a Preliminary Data from 16-foot Wind-Tunnel Tests of the Lockheed. -38 Model. Marley J. Hood. June 13, 1942.

 

(AT-2) 21-30a P-38 1/6 Scale High Speed Wind Tunnel Model Report #LA.L. 17 - Part II. December 16, 1941.

Physical Description: [drawings]
Box Box 270

(AT-2) 21-30a Preliminary Data from 16 foot Wind Tunnel Tests of the Lockheed P-38 Model. Manley J. Hood. September 5, 1942.

 

(AT-2) 21-30a Preliminary Data from 16 ft. Wind Tunnel Tests of Lockheed P-38 Model. Manley J. Hood. June 29, 1942.

 

(AT-2) 21-30a Preliminary Data from 16 foot Wind Tunnel Tests of the Lockheed P-38 Model. Albert L. Erickson. 4, 1942.

 

(AT-2) 21-30a Preliminary Data from 16-foot Wind Tunnel Tests of the Lockheed P-38 Model. Albert L. Erickson. November, 13, 1942.

 

(AT-2) 21-30a Preliminary Data from 16-foot Wind Tunnel Tests of Lockheed P-38 Model. Albert L. Erickson. November 26, 1942.

 

(AT-2) 21-30a Preliminary Data 16 foot Wind Test of the Lockheed P-38 Model. Albert L. Erickson. December 3, 1943.

Box Box 271

(AT-2) 21-40 Tests. XP-56. Northrop Aircraft. 1943.

 

(AT-2) 21-40a Tests. XP-56. Preliminary Results. 1942-1943.

 

(AT-2) 21-40a Preliminary Data on 16 foot Wind Tunnel Tests of Northrop XP-56 Model. Manley J. Hood. September 7, 1942.

 

(AT-2) 21-40a Preliminary Data - II 16 foot Wind Tunnel Tests of Northrop XP-56 Model. Edmund V. Laitone. December 1, 1942.

 

(AT-2) 21-40a Preliminary Data on the 16-foot Wind Tunnel Tests of Northrop XP-56 Model. Edmund V. Laitone. November 26, 1942.

 

(AT-2) 21-45 Tests. XB-29, Boing Aircraft.

Physical Description: [Correspondence reports and drawings]
Box Box 272

(AT-2) 21-45 XB-29.

Physical Description: [Drawings]
Box Box 273

(AT-2) 21-45. XB-29.

Physical Description: [Drawings]
Box Box 274

(AT-2) 21-45 Stress Analysis of XB-29.

Physical Description: [Drawings]
 

(AT-2) 21-45 Tests. XB-29. Boeing. 1943-1945.

Physical Description: [drawings and correspondence Primarily transmittal sheets]
 

(AT-2) 21-45a Preliminary Data - III 16 foot Wind Tunnel Tests of the Boeing XB-29 Airplane Model. Victor M. Ganzer. January 22, 1943.

 

(AT-2) 21-45a Preliminary Data - II 16 foot Wind Tunnel Tests of the Boeing XB-29 Airplane Model. Victor M. Ganzer. January 16, 1943.

 

(AT-2) 21-45a Preliminary Data I 16 foot Wind Tunnel Tests of the Boeing XN-29 Airplane Model. Victor M. Ganzer. January 7, 1943.

 

(AT-2) 21-45a Preliminary Data IV 16 foot Wind Tunnel Tests of Boeing XB-29 Airplane Model. Victor M. Ganzer. January 25, 1943.

Box Box 275

(AT-2) 21-45a Preliminary Data - V 16 foot Wind Tunnel Tests of the Boeing XB-29 Airplane Model. Victor M. Ganzer. January 30, 1943.

 

(AT-2) 21-45a Preliminary Data VI 16 foot Wind Tunnel Tests of the Boeing XB-29 Airplane Model. Victor M. Ganzer, February 2, 1943.

 

(AT-2) 21-45a Preliminary Data - VIII 16 foot (etc XB-29) Victor M. Ganzer February 5, 1943.

Box Box 276

(AT-2) 21-45a Preliminary Data XX (same title/aut) March 24, 1943.

 

as above. Prelim Data XIX, March 22, 1943 [same title/Aut]

 

(AT-2) 21-45a as above. Prelim Data XVIII March 19, 1943 [same title/Auth]

 

as above Prelim Data XVII. March 18, 1943. [same title/Auth]

 

as above Prelim Data XVI [same title] March 13, 1943

 

(AT-2) 21-45a as above Prelim Data XV [same title] March 11, 1943. [Lee J. Boddy]

Box Box 277

(AT-2) 21-45a Prelim Data XIV. same title March 5, 1943. [Lee J. Boddy]

 

(AT-2) 21-45a Prelim Data XIII [same title] February 24, 1943 [Victor M. Ganzer.]

 

(AT-2) 21-45a Prelim Data XII [same title] February 22, 1943. [Ganzer.]

 

(AT-2) 21-45a Prelim Data XI [same title/auth] February 16, 1943.

 

(AT-2) 21-45a Prelim Data X [same title/author] February 15, 1943.

 

(AT-2) 21-45a Prelim Data IX [same title/author] February 13, 1943.

 

(AT-2) 21-45a Prelim Data VII. [same title/author] February 11, 1943.

Box Box 278

(AT-2) 21-45a Prelim Data XXXIII. [same T/A] July 23, 43

 

(AT-2) 21-45a Prelim Data XXXII. [same T/A] July 23, 43

 

(AT-2) 21-45a Prelim Data XXI. [same T/A] July 22, 1943

 

(AT-2) 21-45a Prelim Data XXX. [same T/A] July 21, 1943

 

(AT-2) 21-45a Prelim Data XXIX. [same T/A] June 3, 1943. Robt. H. Barnes

 

(AT-2) 21-45a Prelim Data XXVII. [same T] June 1, 1943 Victor M. Ganzer

 

(AT-2) 21-45a Prelim Data XXVII. [same T/A] May 21, 1943

Box Box 279

(AT-2) 21-45a Prelim Data XXVI. [same T/A] May 5, 1943

 

(AT-2) 21-45a Prelim Data XXV. [same T/A] April 23, 1943

Box Box 280

(AT-2) 21-45c Prelim Data XXIV. [same T] April 12, 1943 Robt. H. Barnes

 

(AT-2) 21-45c P D XXIII. [same T] April 3, 1943 Victor M. Ganzer

 

(AT-2) 21-45c P D XXII. [same T/A] March 31, 1943

 

(AT-2) 21-45c P D XXI. [same T/A] March 27, 1943

Box Box 281

(AT-2) 21-50 Tests XP-58 Lockheed. 1942-1944]

Physical Description: [drawings and correspondence
 

(AT-2) 21-50a Preliminary Results. 1943-1945

 

(AT-2) 21-50a P D, [same T/A] November 3, 1943

 

(AT-2) 21-50a P D Reports, July - October, 1942

Box Box 282

(AT-2) 21-55 Tests C69. Lockheed.

 

(AT-2) 21-55a Tests C-69 Lockheed. Prelim, Results.

 

(AT-2) 21-60 Tests XF5U-1 Vought-Sikorsky. 1944-1945.

Physical Description: [Correspondence Blueprints and drawings]
Box Box 283

(AT-2) 21-60 [Loose blueprints, reports and drawings. 1944]

Box Box 284

(AT-2) 21-60 [Loose drawings. 1944]

Box Box 285

(AT-2) 21-60 [Loose Drawings and Blueprints. 1944]

Box Box 286

(AT-2) 21-65 Tests P-51. North American. 1943-1944.

 

(AT-2) 21-65 [Loose Drawings. 1943.]

Box Box 287

(AT-2) 21-65 [Loose Drawings. 1942-1943]

Box Box 288

(AT-2) 21-65 [Loose Drawings. 1943.]

 

(AT-2) 21-65a P-51- Prelim. Results 1943-1945. [Include Preliminary Data Reports, 1944.

Box Box 289

(AT-2) 21-65a Preliminary Data Reports, May 28, 1943 - September 21, 1944.

Box Box 290

(AT-2) 21-65a Preliminary Data Reports, May 31, 1943 - May 31, 1943.

 

(AT-2) 21-70 Tests XC-97 Boeing. October 1943.

Physical Description: [drawings]
 

(AT-2) 21-70a Tests XC-97 Boeing. Preliminary Results [contains Prelim Data Report, April 14 1943]

Box Box 291

(AT-2) 21-75 Tests in XP-51B Duct Rumble North American. 1943

Physical Description: [correspondence and drawings]
 

(AT-2) 21-75 [Loose drawings]

Box Box 292

(AT-2) 21-75a Tests XP-51B. North American. Prelim Results.

 

(AT-2) 21-75a Preliminary Data Reports, April 3, 1943 - May 19, 1943

Physical Description: [5 folders]
 

(AT-2) 21-80 Tests. XTB2D-1. Douglas. 1943.

 

(AT-2) 21-80 [Loose Blueprints.]

Box Box 293

(AT-2) 21-80 [Loose blueprints and drawings.]

Box Box 294

(AT-2) 21-85 Tests P-47. Republic.

Physical Description: [drawing, reports and blueprints.]
 

(AT-2) 21-85 [Loose blueprints and drawings.]

Box Box 295

(AT-2) 21-85 [Loose blueprints and drawings.]

 

(AT-2) 21-85a Tests P47. Republic. Prelim Results. 1943-1946.

 

(AT-2) 21-85a Preliminary Data. November 1944.

Physical Description: [2 folders]
Box Box 296

(AT-2) 21-85a Preliminary Data. 1943-1945.

Physical Description: [3 folders]
Box Box 297

(AT-2) 21-85a Preliminary Data. 1943-1945.

Physical Description: [8 folders]
 

(AT-2) 21-90 Tests XB-29, Aileron. Boeing. 1943-1945.

 

(AT-2) 21-90a Tests XB-29 Aileron. Boeing. Prelim Results. 1943-1944.

 

(AT-2) 21-90a Preliminary Data. August 1943.

Physical Description: [9 folders]
Box Box 298

(AT-2) 21-90a Preliminary Data. August 1943 - October 1943.

Physical Description: [10 folders]
 

(AT-2) 21-95 Spoiler and Aileron Investigation. A-15. 1943-1944.

 

(AT-2) 21-100 Tests. XFD-1. McDonnell.

Box Box 299

(AT-2) 21-100 [Loose blueprints and drawings]

Box Box 300

(AT-2) 21-100 [Loose blueprints and drawings]

Box Box 301

(AT-2) 21-100 [Loose blueprints and drawings]

Box Box 302

(AT-2) 21-100 [Loose Blueprints and drawings]

Box Box 303

(AT-2) 21-100 [Loose blueprints and drawings]

 

(AT-2) 21-100a Test XFD-1. McDonnell. Prelim. Result.

Physical Description: [Reports, blueprints]
 

(AT-2) 21-100a Preliminary Data. July 19, 1944.

Box Box 304

(AT-2) 21-100a Preliminary Data. July 19, 1944 - September 18, 1944

Physical Description: [9 folders]
Box Box 305

(AT-2) 21-100a Preliminary Data. 1944-1945.

Physical Description: [5 folders]
 

(AT-2) 21-105 Tests. XB-42. Douglas. 1943-1944.

 

(AT-2) 21-105 [Loose blueprints]

Box Box 306

(AT-2) 21-105. [Loose blueprints]

Box Box 307

(AT-2) 21-105a Preliminary Data. February 28, 1944 - March 29, 1944.

Physical Description: [9 folders]
 

(AT-2) 21-110 Tests XA-39. Fleetwings. 1943. Douglas.

Box Box 308

(AT-2) 21-110 [Loose blueprints] Douglas.

 

(AT-2) 21-105a Tests SA-42 Prelim Results.

 

(AT-2) 21-105a Preliminary Data. February 1944.

Physical Description: [3 folders]
Box Box 309

(AT-2) 21-110a [Loose Blueprints] These are for XA-39

Box Box 310

(AT-2) 21-110a Loose blueprints [seem to be XA-39]

 

(AT-2) 21-112 Tests XP-79. Avion Spoilers. October 1943 - Jan. 1944.

 

(AT-2) 21-112a Preliminary Results. contains Preliminary Data Reports. November 10, 1943 - December 13, 1943.

Physical Description: [6 folders]
 

(AT-2) 21-112a A-74. Preliminary Data Reports I - III. (High Speed Tests of an Upper Surface Spoiler on Naca Tapered Wing.) April 29, 1944 - May 5, 1944.

 

(AT-2) 21-115 Tests XP-55. Curtiss-Wright. July 1943 - December, 1943.

Physical Description: [4 folders]
 

(AT-2) 21-115a [Loose drawings and blueprints.]

Box Box 311

(AT-2) 21-115a [Loose drawings and blueprints N.D.C. 1943]

Box Box 312

(AT-2) 21-115a Preliminary Results. December 31, 1943.

Physical Description: contains PD Report.
 

(AT-2) 21-120a Tests XB-42. Full Scales Empennage. Douglas. May 23, 1944 - July 20, 1945.

 

(AT-2) 21-120a Preliminary data reports. May 19, 1944 - August 25, 1944

Physical Description: [11 folders]
Box Box 313

(AT-2) 21-122 Tests XP-81 Consolidated (A-96) May 1944 - May 1945.

 

(AT-2) 21-122 [Loose drawings] 1944

 

(AT-2) 21-122 Table I of XP-81 "Wing Coordinates of XP-81 Airplanes."

Physical Description: [2 folders.]
 

(AT-2) 21-122 [Loose Blueprints] 1944

Box Box 314

(AT-2) 21-122 [Loose blueprints] 1944

Box Box 315

(AT-2) 21-122 [Loose blueprints and drawings] 1944

 

(AT-2) 21-122a High Speed Wind-Tunnel Test of a Model of the Consolidated Vultee XP-81 Airplane - Power Off. by Henry Jessen and Jack K. Stephenson [N.D.]

Box Box 316

(AT-2) 21-122a Tests. XP-81. Consolidated (A-96). January 1945 - July 1945.

 

(AT-2) 21-122a Preliminary Data Reports. Jossen and Stephenson, Jan. 5, 8, 11, 25 (2) 31, Feb. 5.

Physical Description: [7 folders]
Box Box 317

(AT-2) 21-122a Preliminary Data Reports.

Physical Description: [15 folders]
Box Box 318

(AT-2) 21-122a P D reports.

Physical Description: [11 Folders]
Box Box 319

(AT-2) 21-125 Tests. XP-82.

 

(AT-2) 21-125 [Loose drawings]

Box Box 320

(AT-2) 21-125 [Loose drawings]

Box Box 321

(AT-2) 21-125 [Loose drawings]

 

(AT-2) 21-125a Preliminary Results (XP82). 1944-1945.

 

[(AT-2) 21-125a] Process Manual [issued to aerodynamics dept; designed by North American Aviation, re XP82]

 

(AT-2) 21-125a Preliminary Data. April 1946.

Physical Description: [3 folders]
Box Box 322

(AT-2) 21-125a Preliminary Data. December 1944-April 1946.

Physical Description: [12 folders]
Box Box 323

(AT-2) 21-125a Preliminary Data. May 1945 - June 1945.

Physical Description: [8 folders]
Box Box 324

(AT-2) 21-125a Preliminary Data. Feb. 45 - May 45

Physical Description: [8 folders.]
Box Box 325

(AT-2) 21-125a Preliminary Results (contd).

Physical Description: [1 folder]
 

(AT-2) 21-125a Preliminary Data. January 1945

Physical Description: [4 folders]
Box Box 326

(AT-2) 21-125a Preliminary Data. Feb. - June 1945.

Physical Description: [12 folders]
Box Box 327

(AT-2) 21-125a Preliminary Data. March 1945.

Physical Description: [9 folders]
Box Box 328

(AT-2) 21-125a Preliminary Data. March - April 1945.

Physical Description: [5 folders]
Box Box 329

(AT-2) 21-130 Tests P39N-1. Bell. 1944-1945

 

(AT-2) 21-135 Tests XF7F-1 1944-1945

Physical Description: [Little correspondence; primarily blueprints]
 

(AT-2) 21-140 Tests YP-80a. Lockeed. 1944-1945

Physical Description: [Little correspondence; primarily blueprints]
Box Box 330

(AT-2) 21-140 Preliminary Results. February 10, 1945 - July 14, 1947

 

(AT-2) 21-140a Preliminary Data Reports. February 10, 1945 - Sept. 7, 1945.

Physical Description: [11 folders]
Box Box 331

(AT-2) 21-140a Preliminary Data Report. September 18, 1945

 

(AT-2) 21-142 Tests YP-80a. November 6, 1945 - February 13, 1946

 

(AT-2) 21-142a XP-80A Outer Wing Panel. Preliminary Results. 21 January 1946 - 28 March 1946.

 

(AT-2) 21-142a Preliminary Data Reports. January 16, 1946 - February 11, 1946.

Physical Description: [4 folders]
Box Box 332

(AT-2) 21-142a Preliminary Data Reports. 27 February 1946 - March 18, 1946.

Physical Description: [3 folders]
 

(AT-2) 21-145 Tests and Preliminary Results [Wing and Fuselage Studies] 1945-1946.

 

(AT-2) 21-150 Tests BT2D-1. Douglas 1945-1947

 

(AT-2) 21-150a Preliminary Data. March - Dec 1946. for BT2D-1 and AD-1 model

Physical Description: [7 Folders]
Box Box 333

(AT-2) 21-150a Preliminary Data. Dec. 45 - Jan. 46

Physical Description: [6 folders]
 

(AT-2) 21-155a Tests XP-80, Consolidated. April 1, 1944, July 9, 1946.

Physical Description: [2 folders - 1 empty]
 

(AT-2) 21-155a Preliminary Data. March - April 1944.

Physical Description: [4 folders]
Box Box 334

(AT-2) 21-155a Preliminary Data. April - May 1944.

Physical Description: [4 folders]
Box Box 335

(AT-2) 21-155a Preliminary Data. May 1944.

Physical Description: [1 folder]
 

(AT-2) 21-160 Tests XB-43. DaDouglas. 1945

Physical Description: 1 folder
 

(AT-2) 21-160 [Loose blueprints. 1943-1944]

Box Box 336

(AT-2) 21-160 [Loose blueprints and drawings. 1943-1944]

Box Box 337

(AT-2) 21-160 [Loose blueprints 1944.]

 

(AT-2) 21-160a XB 43 Preliminary Results. September 1944 - October 1944.

 

(AT-2) 21-160a S21-25b. Preliminary Data. September 1944.

Physical Description: [2 folders]
Box Box 338

(AT-2) 21-160a S21-25b. Preliminary Data. September 1944 October 1944.

Physical Description: [11 folders]
Box Box 339

(AT-2) 21-160a S21-25b. Preliminary Data. November 1944.

Physical Description: [2 folders]
 

(AT-2) 21-165 [Loose Drawings]

Box Box 340

(AT-2) 21-165 [Loose drawings and blueprints]

Box Box 341

(AT-2) 21-165 [Loose drawings and blueprints]

 

(AT-2) 21-165a Preliminary Data. May 1946 - November 1946.

Physical Description: [6 folders]
Box Box 342

(AT-2) 21-180 Tests CVAC "Lark:. Consolidated. 1945

 

(AT-2) 21-180 [Loose blueprints. 1945]

Box Box 343

(AT-2) 21-180 [Loose blueprints. 1945]

Box Box 344

(AT-2) 21-195 [Transmittal Forms, Blueprints and drawings pertaining to the XP-86. 1946-1947]

 

(AT-2) 21-180 Consolidated Voultee Aircraft Corporation Lark. 1945.

Physical Description: [Drawings]
 

(AT-2) 21-180a CVAC Lark. Preliminary Results.

Physical Description: [empty folder]
 

(AT-2) 21-180a Preliminary Data Reports. October - December, 1945.

Physical Description: [6 folders]
Box Box 345

(AT-2) 21-180a Preliminary Data Reports. December 1945 - January 1946.

Physical Description: [5 folders]
 

(AT-2) 21-180a NACA Research Memorandum - A6K19 For the Bureau of Aeronautics, Navy Department. December 13, 1946. Lark Missile

Box Box 346

(AT-2) 21-185. Tests P51 H. Stabi(lity) and Control. North Am, Avia. November 1945 - December 1945.

Physical Description: [little correspondence, primarily drawings]
Box Box 347

(AT-2) 21-185 [Loose drawings]

Box Box 348

(AT-2) 21-185 [Loose drawings]

 

(AT-2) 21-195 Tests XP-8-8.

Physical Description: [empty]
 

(AT-2) 21-195 [Drawings.]

Box Box 349

(AT-2) 21-195 [Loose drawings]

Box Box 350

(AT-2) 21-195 [Loose drawings]

Box Box 351

(AT-2) 21-210 Test. C.74. Douglas 1946-1947

 

(AT-2) 21-210a Preliminary Results.

Physical Description: [empty]
 

(AT-2) 21-210a Preliminary Data. September 6, 1946 - January 17, 1947.

Physical Description: [8 folders]
 

(AT-2) 21-210a NACA Research Memorandum No A7028 for the Air Material Command, Arny Air Force. May 6, 1947.

 

(AT-2) 21-230 Tests. XF2H-1. McDonnell. 1947

Box Box 352

(AT-2) 21-230 Tests. XF2D-1. McDonnell. 1946

Physical Description: [Loose drawings blueprints and correspondence]
 

(AT-2) 21-230 Stress Analysis 2/7 Scale High Speed Wind Tunnel Model XF2D-1. Report No. 340 Serial 4. November 1, 1945.

 

(AT-2) 21-230 [Loose drawings 1945]

Box Box 353

(AT-2) 21-230 [Loose drawings 1945]

 

(AT-2) 21-230 Reprot No 340. Serial 5. November 1, 1945.[with attached drawings]

 

(AT-2) 21-235 Tests-Wing tip-mounted tuit (A-216). 1944-1947.

 

(AT-2) 21-240 Tests-Douglas XS-3. (A-218) 1948.

Box Box 355

(AT-2) 21-245 High Speed Tests Fairchild. XSDM-2. (Lark) Pilotless Aircraft. (A223) 1949.

Box Box 356

(AT-2) 21-250a MX-838. 16th. Preliminary Results. RA A-233. 1948

Box Box 357

(AT-2) 21-265a Prelim Results. 1/6 Scale Bumblebee XPM Model (JOHNS HOPKINS UNIV). RA A271. (1949)

Box Box 358

(AT-2) 21-275 HS WT Inv. of Arodynamic Char. of Boeing XB-52 `plane. (C) 16' AMC. (RAA-256). 1950/

 

(AT-2) 21-280. Tests. "HS WT Invest of Horizontal Tail of Northrop F-89 Plane". (RA-258) (C). 1950

Box Box 359

(AT-3) 5-20 Equipment, General. 1944-1947.

 

(AT-3) 5-20a Equipment - Smoke Generating (1944-1947)

 

(AT-3) 16-30 Operations, General. 1944-1950.

 

(AT-3) 17-20 Research Programs. General 1944-1945

 

(AT-3) 19-15 Research Problems Suggested. 1944-1948

Box Box 360

(AT-3) 21-5 Tests - General. 1943-1945.

 

(AT-3) 21-5b Tests - Progress Reports and Tunnel Schedules 1944-1946.

 

(AT-3) 21-10 Tests. BTD-1. Douglas. 1944-1945.

 

(AT-3) 21-10 [Loose blueprints and drawings] June 1945 - January 1946.

 

(AT-3) 21-10a Preliminary Data Reports. September 2, 1944 - November 28, 1944.

 

(AT-3) 21-25a Preliminary Data Northrop N9M-2 October 31, 1944 - February 26, 1945.

Box Box 361

(AT-3) 21-10a Preliminary Results BTD-1 October 23, 1944 - June 29, 1945.

 

(AT-3) 21-25a Tests. N9M-2. No thrip November 2, 1944 - March 3, 1945.

 

(AT-3) 21-30 Grumman XFTF-1 1944-1945.

Physical Description: [Correspondence, loose drawings, blueprints.]
 

(AT-3) 21-30a XG7F-1. Preliminary Results.

Physical Description: [empty]
Box Box 362

(AT-3) 21-30a Preliminary Data Reports. October 2, 1944 - January 5, 1945.

Physical Description: [12 folders]
Box Box 363

(AT-3) 21-30a Preliminary Data Reports. January 19, 1945 - July 5, 1945

Physical Description: [15 folders]
 

(AT-3) 21-35 Tests. XP-56. Northrop 1944-1945.

Box Box 364

(AT-3) 21-40 Tests. P75. General Motors. 1944-1945.

Box Box 365

(AT-3) 21-40 [Loose blueprints and drawings]

Box Box 365

(AT-3) 21-40a Preliminary Results. [contains 6 P D Reports. January 6, 1945 - August 9, 1945. Also a copy of NACA Memorandum Report for Air Technical Services Command, USAAF. dated November 7, 1945.]

Box Box 366

(AT-3) 21-55 Tests FR-1. Ryan. 1945.

 

(AT-3) 21-55 [Loose blueprints]

Box Box 367

(AT-3) 21-55 [Loose blueprints and drawings]

 

(AT-3) 21-55a Tests FR-1 Ryan (A-153) Preliminary Results. [Contains P D Reports - March 30, 1945 - July 31, 1945

Physical Description: 14 folders
Box Box 368

(AT-3) 21-60 Tests XBT 2D-1, Douglas. 1945.

Box Box 369

(AT-3) 21-60 [Loose blueprints May 1945]

 

(AT-3) 21-60a XBT2D-1 Preliminary Results.

 

(AT-3) 21-60a Preliminary Data Reports. July 26, 1945 - December 17, 19

Physical Description: [10 folders
Box Box 370

(AT-3) 21-60a Preliminary Data Reports. April 17, 1947 -October 10, 1945 October 18, 1945;

Physical Description: [3 folders]
 

(AT-3) 21-65a Test A-26B. Douglas. May 21, 1945 - July 20, 1945.

 

(AT-3) 21-65a Preliminary Results. Contains P D Reports, 18 May 45-26 June 45.

Physical Description: 15 folders
Box Box 371

(AT-3) 21-70 Tests FR-1 Engineering Division (A-168) 1946.

 

(AT-3) 21-70 [Loose blueprints]

Box Box 372

(AT-3) 21-70 [Loose drawings and blueprints]

Box Box 373

(AT-3) 21-70 [Loose drawings]

Box Box 374

(AT-3) 21-70 [Loose drawings]

Box Box 375

(AT-3) 21-70 [Loose drawings]

Box Box 376

(AT-3) 21-70 [Loose drawings]

Box Box 377

(AT-3) 21-70 [Loose drawings and blueprints]

Box Box 378

(AT-3) 21-70 FR1. Preliminary Results. [Contains 4 PD Reports July 9, 1945 - August 11, 1945]

 

(AT-3) 21-75 Tests XB-36. Consolidated Vultee. 1945-1947.

 

(AT-3) 21-75 a Preliminary Results [Contains PD Reports Septmeber 26, 1945 - December 3, 1945

Physical Description: 4 folders]
 

(AT-3) 21-80 Tests Parachute. 19 June 1945. [only contains one transmittal statement]

 

(AT-3) 21-85a FR-1 Preliminary Results [Contains 5 PD Reports.] January 9, 1946 - January 15, 1946

 

(AT-3) 21-110a Air Intake Ducks Preliminary Data Report November 7, 1946

 

(AT-3) 21-125 Tests XP-91, Republic May 14, 1947 - July 7, 1947

 

(AT-3) 21-125 [Loose blueprints, drawings. 1942-1948]

Box Box 379

(AT-3) 21-125 [Loose drawings 1946-1947]

 

(AT-3) 21-125a Tests XP-91 Preliminary Results [Contains 9 PD Reports dtd May 9, 1947 - Oct. 22, 1947]

Box Box 380

(AT-3) 21-125a [Loose blueprints 1945-1946.]

Box Box 381

(AT-3) 21-125a [Loose blueprints, 1946-1947]

Box Box 382

(AT-3) 21-125a [Loose blueprints, drawings 1946-1947]

Box Box 383

(AT-3) 21-130 40 x 80. RAA-199/ (1946-1948).

 

(AT-3) 21-145 Tests - Invest. of Full Scale Charac. of Con. Vultee XP-92 (A-210). [1948]

 

(AT-3) 21-150 Test - 40-by 80 ft. Wind-Tunnel Inv. of McDonnell XP-85 Airplane. (A-211).

 

(AT-4) 1-10 Airfoils - General. 1948

 

(AT-4) 1-10 Airfoils - General. 1943-1946

 

(AT-4) 5-10 Equipment. General. 1945

 

(AT-4) 21-10a P.D. "Pressure-Distribution Measurements at High Speeds for Five Representative NACA Low-Drag and Conventional Airfoils." April 30, 1945.

Box Box 384

(AT-5) 21-5b Tests. Progress Report. [1945-1949]

 

(AT-5) 21-15a Tests. Progress Report. [1945-1949]

 

(AT-5) 21-20 Tests-Aerody. Char. of Ducts and Duck Inlets. [1947]

 

(AT-5) 21-25 Supersonic Inv. Lockheed Ram Jet Test Vehicle. (RAA-226) (1948)

Box Box 385

(AT-6) 5-10 Equipment - General. [1949]

 

(AT-6) 21-40a Prelim. Results. (A-236)

 

(AT-7) 5-10 Equipment - General. [1949]

 

(AT-10) 9-10 Investigations General. [1948-1950]

Box Box 386

(AT-11) 3-20 Computations - General. [1949]

 

(AT-11) 9-5 Inquires. Commercial Sources. [1949]

 

(AT-11) 3-20a Computations - Reeves Electronic Analog Computers. (REAC). [1948-1949]

 

(AT)17 17-20 Propellers 1951. Drawings. Budget (General). 1941-1950. [1951]

 

B1-5 Allotments - General. [1945]

 

B1-5a Allotments - C&E Funds. [1945]

 

B1-5b Allotments - General Funds. [1945]

 

B1-10 Appropriations - Estimates of. [1945]

 

B1-12 Budget - Fiscal Year 1954.

Box Box 387

B2-20 Budget - 1945 - General.

 

B2-20a Budget - 1945 - Supplemental Estimate

 

B2-21 Budget - 1946 - General

 

B2-21 Ames Aeronautical Laboratory Fiscal Year. 1946. August 7, 1944.

 

B2-21a Budget - 1946 - Supplemental Estimates.

Box Box 388

B2-22a Budget - 1947 - Memos to Divisions and Sections.

 

B2-22b Budget. [Samples to be used in preparing project requests). [1947]

 

B2-22b Budget - 1947. Instructions for Wash. Office.

 

B2-22c. Budget - 1947 - Rough Draft.

 

B2-22d. Ames Aeronautical Laboratory. Fiscal Year 1947. Estimates. August 3, 1947.

 

B2-22d. Budget - 1947 - Final Budget.

Box Box 389

B2-22e. Budget - 1947 - Supplemental Estimate

 

B2-22f. Construction Program thru Fiscal Year. 1952.

 

B2-22g. Ames Aeronautical Laboratory. Fiscal Year 1948. Estimates. August 12, 1946.

Box Box 390

B2-22g. Budget - 1948.

 

B2-22h Budget - 1949.

 

B2-22i. 1950 Budget.

Box Box 391

B2-22j. Budget. 1951.

 

B2-22k. Budget. 1952.

 

B2-22l. Budget. 1953.

 

B2-40. Bureau of Budget - Memos, etc. [1941-1951]

 

B2-45. Budget - Muroc. [1949]

 

B3-5. Cost Analysis. [1946-1948]

 

B16-10. Obligation Breakdown. [1945-1946]

 

B19-10. Reports. [1945-1946]

Box Box 392

C-2-1. A2. McDonnell. F3H. 1953.

 

C-2-1. A2. Flight Investigation of Buffeting of High Speed Aircraft

 

C-2-1. A5. Flight Inv of Horizontal Tail Loads F-86A. Airplane and F-86D ' plane Lowered Horizontal Tail Position. (c). [1954]

 

C-2-1. A7. Division of Load Between Wing and Body at Transonic Speeds. [1952-1955]

 

C-2-2. A6. Investigation of Critical Maneuvers and Loads Resulting There from During Flight Test of a Swept-Wing Airplane. [1952-1955]

 

C-2-3. A3. Wind-Tunnel Investigation of the Mechanism of Buffeting at Subsonic Speeds. [1952-1955]

 

C-2-3 A8. Gust Responses of Elastic Wings at Supersonic Flight Velocities. [1953-1955]

 

C-3-2. A4. Determination of Flutter Derivatives at Transonic Speeds. [1955]

 

C-3-2. A7. Determination of Elastic and Geometric Characteristics for Flutter of Straight Wings at Transonic Speeds. [1952-1955]

 

C-3-3. A5. Investigation of the Cause of Failure of the Northrop F-89 Elevator. [1952]

 

C-3-3. A6. Investigation of Elevator Oscillation of Northrop F-89 Airplane. (C) [1951]

Physical Description: 1 x 3½.
 

C-3-4. A10. Analysis of Existing Fluctuating Pressure Data on Two-Dimensional Airfoils. [1954-1955]

 

C-46. Summary of a Number of Reports on Thermal Ice Prevention. 1949.

Box Box 393

E1-1 Agard - General. 1954. [Advisory Group for Aeronautical Research]

 

E1-1 Agard - Paris, France, November 1954.

 

E1-1 Agard - Netherlands, May 1954.

Box Box 394

E1-1a. Accidents - Airplanes. 1949.

 

E1-5. Aeronautical Board. 1942-1947.

 

E1-10a. Aircraft - British. 1941-1946.

 

E1-10a. Aircraft - British. 1947-1948.

 

E1-10b. Aircraft - German. 1947-1948.

 

E1-12. Annual Inspection - Ames. 1946.

Box Box 395

E1-12. Annual Inspection - Ames. Mar - June 1948

 

E1-12. Annual Inspection - Ames. July - 1948

 

E1-12 Annual Inspection - Ames. 1946.

 

E1-12b. Annual Inspection - Cleveland. 1947-1948

Box Box 396

E1-12a Annual Inspection - Langley. 1947.

 

E1-12a Annual Inspection - Langley. 1949.

 

E1-12 Annual Inspection - Langley. 1950

Box Box 397

E1-12a [Copies of Material Presented at the 1949 Biennial Inspection. Langley.

Physical Description: 17 folders]
Box Box 398

As Above

Box Box 399

E1-15 Army Air Forces-Material Command Center. 1948.

 

E1-15. Army Air Force-Material Command Center [1943-1948]

Box Box 400

E1-15. Aerojet Engineering Corp. 1952-1954.

 

E1-15. Air Force - General. 1949

 

E1-15. Air Force - General. 1950

 

E1-15a Air Force. Liasison Officer at Ames. 1947-1948.

 

E1-15a Army Air Force Reports. (General). [1943-1947]

 

E1-15b. Edwards Air Force Base. 1945-1948.

 

E1-15c. Army Air Forces - Research Authorizations. 1947-1948.

 

E1-18. Atomic Energy Commission. 1947-1948.

 

E1-20. Avion Inc.

Physical Description: 1 Folder
 

E2-5 Bell Aircraft, Inc.

Physical Description: 1 Folder
 

E2-10. Boeing. 1944. 1947

Physical Description: 1 Folder.
Physical Description: 1 Folder
 

E1-20. Aerolab Development Co. 1951-1952.

Box Box 401

E1-30. Aircraft Industries Assoc. 1950-1953

 

E1-30 Aircraft Industries Assoc. 1954.

 

E1-30 [Actually 31] Aircraft Industries Assoc. 1954.

 

E1-40. Air Force - General. 1953-1954.

 

E1-40. Air Force - General. 1950-1953.

 

E1-40. Air Force - General. 1945-1946

 

E1-40b Air Force. Report of Research. Projects at Ames. 1954.

Box Box 402

[As above. 1953. 1952.

Physical Description: 2 folders]
 

E1-40d Research Authorizations. Transmitted to AFDFR. 1954-1956

 

E1-40d. R.A.'s transmitted to AFDFR. 1949-1953

 

E1-40e. [Air Force - Availability of Air Force Aircraft] 1954-1955.

 

E1-40f. Air Force - WADC - Wright Air Development Center. 1954.

 

E1-40f WADC 1950 - 1953

Box Box 403

E1-40g. ARDC. 1954

 

E1-40g. ARDC. 1952-1953.

 

E1-40h. Arnold Eng. [ineering] Dev. [elopment] Center. 1954.

 

E1-40h. AEDC Transonic Subcommittee Meetings

 

E1-40h. Arnold Eng. Dev. Center. 1950-1953.

 

E1-40h AEDC Transonic S/C Meetings. 1952-1953.

 

E1-55 Army - General. 1951-1954.

 

E1-55c. Balistic Research Lab. 1954.

 

E1-55c. Army Ballistics Res. Lab. Aberdeen. 1949-1953.

 

E1-60. Aro, Inc. 1954

 

E1-60. Aro, Inc. 1952

Box Box 404

E1-65. AEC. 1949

 

E2-4 BAY AREA COUNCIL [1955]

 

E2-20. Bell Aircraft. 1949-1952

 

E2-20. Bell Aircraft. 1954.

 

E2-30. British Air Commission, Washington D.C. (1941-1948.

Box Box 405

E2-35. British Visitors, General. (1941-1948.

 

E2-35a. British Air Ministry [1941-1946]

 

E2-35a British Air Ministry Rpts. (1946-1949).

 

E2-40. Boeing. 1954.

 

E2-40. Boeing. 1953.

 

E3-10. Chamberlain, E.H. [1940-1945]

 

E3-10. Cessna Aircraft. 1954.

Box Box 406

E3-13 Chance Vought

 

E3-13 Chance Vought Aircraft Co. (1945 thru 1948)

 

E3-15 Civil Aeronautics Admin, Board

 

E3-15 Civil Aeronautics Admin, 1948

 

E3-15a Civil Aeronautics Admin, 1942]

Physical Description: [1 folder,
 

E3-15a Civil Aeronautics Admin. 1948

 

E3-20 Chance-Vought. 1954

 

E3-20 Chance-Vought. 1949-1953

 

E3-20. Commission - Air Policy. 1947-1948.

 

E3-25. Civil Aero Admin. 1949-1953.

 

E3-25. Committees - AAL - General. 1942-1946.

Box Box 407

E3-26. Committees, Langley (General). [1945-1947]

 

E3-26. Committees, - LAL - General. - 1948.

 

E3-26. Langley - Minutes of Comm. Meetings Held at Langley. (1949).

 

E3-26. Civil Aero. Board. 1952-1953.

 

E3-26a Committees - LAL - Stability Control. 1948.

Box Box 408

E3-26a Committees, Stability and Control. [1941-1947]

 

E3-26b. Cowling and Cooling (Langley). [1941-1945]

 

E3-26c. aerodynamic. (General) Langley Committee. [1941-1947]

Box Box 409

E3-26c Committees - LAL - Aerodynamic - General. 1948.

 

E3-26d. Committees - Instruments, LMAL. [1944-1945]

 

E3-32 Committee, High Speed Panel

 

E3-32 Committee and Sub Committee General. 1941-1948

 

E3-32 Committees - NACA Committees, Sub Committees and Sub Committee Panels. (1949)

Box Box 410

E3-32a Committees - Induction System De-Icing. [1941-1946]

 

E3-32a-1. Research Airplane Panel. (1948)

 

E3-32a-2. S/C Aircraft Structure. (1948) 1949]

Physical Description: [2 Folders.
 

E3-32a-2 S/C Aircraft Structure. (1949)

 

E3-32a-2 Committee on Aircraft Construction. (1948)

 

E3-32a-2 As above. (1949)

 

4. Supersonic Facilities Panel (1948-1949)

 

5. Committee on power plants for aircraft (1948)

Physical Description: 2 folders
Box Box 411

E3-32b Committees. Lighting Hazards to Aircraft. 1941-1946.

Box Box 412

E3-32a-6 S/C on Fluid Mechanics (1949-1950)

 

E3-32b-1. S/C on Upper Atmosphere. (1948).

 

E3-32b-2 Subcommittee on Aircraft Fire Prevention (1948)

 

E3-32c. Committees - Subcommittee on Meteorlogical Problems (1949).

 

E3-32c S/C - Meterological Problems. 1941-1948.

 

E3-32c Conferences - NACA - Executive Conference. (1943-1950)

 

E3-32d S/C - De-Icing Problems. 1947-1948.

 

E3-32E. Committee - Heat Exvhangers. [1943-1947]

Box Box 413

E3-32f. S/C on Propellers for Aircraft. (1948).

 

E3-32f. Committees - Subcommittees on Propellers for Aircraft (1949).

 

E3-32f. Committees - Propellers for Aircraft. [1944-1948]

 

E3-32g Committee - Aerodynamics [(1944-1946)]

Box Box 414

E3-32g. [Loose Reports and Correspondence. NACA Mtgs. 1946-1947]

 

E3-32g Committees - Committee on Aerodynamics (1949)

Box Box 415

As above. (1948)

 

E3-32h. S/C Vibrations and Flutter. (1948).

Box Box 416

As above (1947)

 

As above (1949)

 

E3-32h. Special Comm on Surplus Aircraft Research. 1946.

 

E3-32i. Subcommittee on Helicopters (1949)

 

E3-32i. S/C on Helicopters (1943 and 1948)

Box Box 417

E3-32j Committee on Operating Problems. (1949).

 

E3-32j. As above. (1948)

 

E3-32j. Committee Operating Problems. [December 7, 1942 - December 12, 1947]

Box Box 418

E3-32k. Committee on Military Operational Data. (1945)

 

E3-321. S/C - Self propelled Guided Missiles. 1946.

 

E3-32m. Committee, Industry Consulting. Oct. 4, 1945 - Dec. 3, 1947.

 

E3-32n. Committees - Special Buffeting Panel (1949).

 

E3-32o. S/C Stability and Control. 1948

Box Box 419

E3-32o. Committee, Stability and Control. Jan 19, `46 November 7, 1947.

 

E3-32o. Committee, Subcommittee on Stability and Control. (1949)

Box Box 420

E3-32p. Committee, High Speed Aerodynamic. Jan 19, 1946 - Oct. 22, 1947.

 

[As above.] (1949)

Box Box 421

E3-32p. S/C High-Speed Aerodynamics. 1948.

Box Box 421A

E3-32p S/C High Speed Aerodynamics. 1948

Box Box 422

E3-32q. Committees, Seaplanes. March 19, 1946 - Oct 1, 1946.

 

E3-32q. Committees, on Aerodynamics, 1948.

 

E3-32q. Committees - Subcommittee on Seaplanes. (1949).

 

E3-32r. Aerodynamics & Structures Panel, Guided Missiles Committee. (1946)

Box Box 423

E3-32s. Propulsion Systems. 1946-1949.

 

E3-32t. High Speed Panel. (1948).

 

E3-32t. Committess. Meeting of NACA High Speed Panel (1949)

 

E3-32u. S/C on Internal Flow. (1948).

 

E3-32u. Committees S/C on Internal Flow. (1949).

Box Box 424

E3-32v. S/C on Aircraft Loads. (1948).

 

E3-32v. S/C on Aircraft Loads. (1949)

 

E3-32x. Special S/C Research Problems of Transonic Aircraft Design. 1948-1949.

Box Box 425

E3-32y. S/C on Icing Problems. (1948).

 

E3-32y. S/C on Icing Problems. (1949)

 

E3-35. Classification. 1951.

Box Box 426

E3-35. Classification. 1952.

 

E3-35. Classification. 1953.

Box Box 427

E3-35. Classification. 1954.

 

E3-35. Classification. 1955.

Box Box 428

E3-35. Conferences, General. (September 9, 1940 - Jan 8, 1948)

 

E3-35. Conferences - General. (1947-1948).

 

E3-35. Conferences - Upper Atomosphere. Rocket Research Panel. (1948).

 

E3-35a Conference, Propellers. July 10, 1941 -March 7, 1947.

 

E3-35b Conferences - Liquid Cooled Air Engine Instruments. dated 11 Sept 41]

Physical Description: [1 item
Physical Description: 1 Folder
 

E3-35c Conferences - Development of Research Instruments. August 2, 1944 - July 24, 1947.

Physical Description: 1 Folder
 

E3-35d. Conferences - NACA. Administrative Conference (1944-1947).

 

E3-35f. Conferences - Lab. Conf. on Flight Techniques. (1944).

Box Box 429

E3-35f. Conferences - Flight Techniques. (September 1, 1944- June 23, 1945.)

 

E3-35h. Personal Aircraft Conf. at Langley. (1946).

 

E3-35i. Stability Control. (Joint NACA. LAL. Ames - Nov 26 & 27th, 1945). (1945 - 1946)

 

E3-35j. Flutter & Vibration Conference at LAL - April, 1946. (1946-1947).

 

E3-35k. Supersonic Aerodynamics Conference at Ames. (1946)

 

E3-35k-1. Supersonic Aerodynamics Conference at Ames. (1947).

Box Box 430

E3-351. Conference- Aviation Writers Assn. (1946-1947).

 

E3-35m. Ice Prevention Conference. (1947).

 

E3-35n. Conference - Boundary Layers (1947-1948).

 

E3-35o. Conferences - Aerodynamic Problems of Transonic Airplane Design. (1947-1948).

 

E3-35p. Conferences - Aircraft Loads - LAL - (1948). (1947-1948).

Box Box 431

E3-35q. [Enclosures Detached from Memos for Director. October 24, 1947.]

Box Box 432

E3-35r- Conferences - NACA. University Conf. on Aerodynamics. LAL - June 21, 22, 23. (1948).

 

E3-35s- Conferences - Aircraft Structure - LAL. (1948).

 

E3-35t. Conferences - NACA Conference on Supersonic Aerodynamics - (Ames - Feb. 28 and March 1, 1950.

 

E3-35t. Superior Conference. Ames. (1948)

Box Box 433

E3-35u. Conferences - NACA Conference on Propellers for Aircraft (Langley - Sept 29, 1949).

 

E3-35v. Conference on Aerodynamic Problems of Transonic Airplane Design. (Langley - Sept 27-29, 1949).

 

E3-35w. Conferences. Navy Conference on Lateral Dynamic Stability Problems and Research (NACA Hdqtrs. - 10/5/49).

 

E3-35x. Conferences - NACA Conference on Some Problems of American Operation. (Lewis - October 9-10, 1950)

Box Box 434

E3-35y. Conferences - USAF - RDB Symposium on the Aerodynamics of Ram Jet Supersonic Inlets. (WADC - Oct. 3-4, 1950).

 

E3-35y-1. Conferences - Computing. (1947-1948).

 

E3-35y-1. Conferences - Computing. (1949)

 

E3-35z. Conferences - Bu Aer - Sperry - SPARROW Conference. (Bu Aer, Wash. - Oct. 17-18, 1950).

 

E3-40. Consolidated Vultee Aircraft Corp. (1948).

 

As above. (1949).

 

E3-40. As above. October 27, 1941 - December 9, 1947.

Scope and Content Note

General Correspondence re models, instruments and supersonic wind tunnel tests.]
Box Box 435

E3-40a. Meeting Scheduled. 1950-1953.

 

E3-40a. Meeting Scheduled. 1954

 

E3-41. Committee on Aircraft, Missile, & Spacecraft on Aerodynamics. 1954.

 

E3-41. Committee on Aerodynamics. 1953 1951-52

Physical Description: [2 folders]
Box Box 436

E3-41. Committee on Aerodynamics. 1950.

Box Box 437

E3-41a. Subcommittee on Fluid Mechanics. 1954.

Physical Description: [2 folders]
Box Box 438

E3-41b. S/C on Hi Sp. Aero. Gen Cases. 1950.

 

E3-41b. Committees - S/C on High Speed Aerodynamics. 1950

Box Box 439

E3-41b. S/C on Hi-Sp Aero. Minutes of Meeting. 1951.

 

E3-41b. S/C on Hi-Sp Aero. Minutes of Meeting. 1952.

 

E3-41b. S/C on Hi-Sp Aero. Minutes of Meeting. 1953.

Box Box 440

E3-41b. S/C on High-Speed Aerodynamics. 1954.

 

E3-41b-1. High Speed Panel. S/C on High Speed Aerodynamics. 1950-1954.

 

E3-41b-2. Subcommittee on High Speed Aerodynamics. Panel on Laminar - Flow Boundary - Layer Control. 1954.

 

E3-41c. Subcommittee on Aerodynamic Stability and Control. 1954.

 

E3-41e. S/C on Internal Flow. 1949.

 

E3-41e. Committees. Subcommittee on Internal Flow. 1954

 

E3-41e. S/C on Internal Flow. Gen Corres. 1950-1953.

Box Box 441

E3-41e. S/C on Internal Flow. Minutes of Meeting. 1950

 

E3-41e. S/C on Internal Flow. Minutes of Meeting. 1951

 

E3-41e. S/C on Internal Flow. Minutes of Meeting. 1953

 

E3-41e. S/C on Internal Flow. Minutes of Meeting.

 

E3-41e. Special West Coast Panel on Air Inlets. 1951.

Box Box 442

E3-41f. Committees - S/C on Propellers for Aircraft 1954-2955, 1953

Box Box 443

E3-41f. Committees - S/C on Propellers for Aircraft. 1952.

 

[As above. 1951]

 

[As above. 1950]

 

E3-41f. S/C on Propellers for Aircraft. 1954

 

E3-41f-1. Panel on Vibration. 1954.

 

E3-41g. S/C on Seaplanes. 1950-1953.

 

E3-41h. S/C on Helicopters. 1950-1953.

Box Box 444

E3-41h. Subcommittee on Helicopters. 1954

 

E3-41i. Committees. Speacial S/C on the Upper Atomosphere (1950-1951).

 

E3-41j. S/C on Stability and Control. Gen. Corres. 1952-1953.

 

[As above. 1950-1951.]

Box Box 445

E3-41j. S/C on Stability and Control - Minutes of Meetings. 1951.

 

[As above. 1952.]

 

[As above. 1953.]

Box Box 446

[As above. 1954.]

 

E3-41j. S/C on Stability & Control. 1951.

 

E3-41j. S/C on Stability & Control. 1950

 

E3-42. Comm on Power Plants for Aircraft. 1954.

 

E3-42. Committee on Power Plants for Aircrafts. 1950-1953.

Box Box 447

E3-42a. Committees - S/C on Aircraft Fuels. (1950-1953.

 

E3-42b. Committees. Subcommittees on Combustion (1953-1954)

 

E3-42b. Subcommittee on Combustion. 1954.

 

E3-42e. Subcommittee on Engine Performance and Operation. 1954.

 

E3-42e. S/C on Engine Performance. 1951-1953.

 

E3-42f. Subcommittee on Power Plant Controls. 1954.

 

E3-42h. Subcommittee on Rocket Engines. 1954.

 

E3-42h. S/C on Rocket Engines. 1953.

 

E3-43. Committee on Aircraft Missile and Space-Craft Construction. 1954.

Physical Description: [Project Zemal]
 

E3-43. Committee on Aircraft Construction. 1950-1953.

Box Box 448

E3-43a. Subcommittee on Aircraft Structure. 1954.

 

E3-43a. S/C on Aircraft Structures. 1950-1952

 

E3-43b. Subcommittee on Loads. 1954

 

E3-43b. Committees - S/C on Aircraft Loads. (1953).

Box Box 449

E3-43b S/C on Loads. 1953

 

[As above. (1952).]

 

[As above. (1951).]

Box Box 450

[As above. (1950).]

 

E3-43c. Committees - S.C on Vibration and Flutter (1953).

Box Box 451

E3-43c. Subcommittee on Vibration and Flutter. 1954.

 

[As above. (1952).]

 

[As above. (1951).]

 

[As above. (1950).]

 

E3-43d. S/C on Aircraft Structural Material. (1950)

Box Box 452

E3-44. Committee on Operating Problems. (1950-1953).

Box Box 453

E3-44 Minutes of the Meeting. Committee on Aircraft & Operating Problems. 1954.

 

E3-44a. Committees - S/C on Meterological Problems. (1950-1953).

 

E3-44b. S/C on Icing Problem. 1954

 

E3-446. S/C on Icing Problem. on Icing Problems. (1950-1953).

 

E3-44d. S/C on Aircraft Noise. 1952-1953.

 

E3-44d. Subcommittee on Aircraft Noise. 1954.

 

E3-44e. Panel on Aircraft Accident Survival. 1952-1953.

 

E3-44e. Panel on Aircraft Accident Survival. 1954.

Box Box 454

E3-44f. S/C on Aircraft Fire Prevention. 1949-1953.

 

E3-44f. Subcommittee on Aircraft Fire Prevention. 1954.

 

E3-50. Coordinator of Research Memos. [1940-1947]

Physical Description: 1 folder
 

E3-60. Curtis - Wright Corp & Cornell Aero Lab [1940-1947]

Physical Description: 1 folder
 

E3-60 Curtis - Wright (Cornell Aero Lab) 1948. [1940-1947]

Physical Description: 1 FOLDER
Box Box 455

E3-60 Conferences, General. 1950-1953

Box Box 456

E3-60. Conferences - General. 1954.

 

E3-60. Conferences. 1950-1951

 

E3-60a-1. Conferences - Aircraft Loads and Structures. (Langley - March 5-7, 1951).

 

E3-60a-2. Conferences - Turbine Materials & Cooling (Lewis 15, Mar. 1951)

Box Box 457

E3-60a Conferences - Aerodynamic Design Problems of Supersonic Guided Missiles (Ames, Oct. 2,3, '51).

Box Box 458

E3-60c-4. Conferences - Aerodynamics of High Speed Aircraft (Ames - July 8-10, 1953)

Box Box 459

E3-60a-4. Conferences. High Speed Airplane Aerodynamics. (Langley - Dec. 4-5, 1951).

Box Box 460

EG-60b-1 Conferences - Supersonic Missile Propulsion. (Lewis - March 13, 1952).

 

EG-60c-1. Conferences - Transonic Wind Tunnel. (Hdqts. - Nov. 2, 1953)

 

E3-60c-2 Conferences - Turbo jet Engines for Supersonic Propulsion. (Lewis - Oct. 8-9, 1953).

 

E3-60c-3. Conferences - Aircraft Loads, Flutter and Structures. (Langley - March 2-4, 1953).

Box Box 461

E3-60d-1. Conferences - NACA, BUAER, WADC, Airplane Flight Control Systems. (March 22-23, 1954).

 

E3-60d Conferences - Helicopters. (Langley; May 12-13, 1954)

 

E3-60d-3. Conferences - Aerodynamics, Structures, and Propulsion (Lewis - Oct. 20-22, 1954).

Physical Description: [incld 1 booklet]
 

E3-60d-4 Conferences - Some Problems of Aircraft Operations (Lewis - Nov. 17-18, 1954)

Box Box 462

E3-60e-3. Conferences - Aerodynamics of Powerplant Installations for H.S. Aircraft (Lewis Proposed) 1954.

 

E3-65. Consolidated Vultee Corporation (Convair). 1954.

 

E3-65. Consolidated Vultee Corporation (Convair). 1950-1953

 

E3-65 Convair. (1953).

 

E3-70. Curtiss-Wright Corp. 1942-1949.

 

E3-90. Curtiss-Wright Corp. 1954.

 

E3-90. Curtiss-Wright Corp. 1950-1953

Box Box 463

E3-90. Curtiss-Wright Corp. 1953

 

E4-5. Department of Defense. 1949-1953.

 

E4-5. Department of Defense. 1954

 

E4-20. Douglas Aircraft Company, Inc. 1954.

 

E4-20. Douglas Aircraft Company, Inc. (1950-1953)

 

As above. 1953. Box 537. As Above. Flight Reports. 1948-1950

 

E4-40. Douglas Aircraft Co, Inc. (1948)

 

E4-40. Douglas Aircraft Co, Inc. (1944-1949)

Box Box 464

E4-40. Douglas Aircraft Co, Inc. 1941-1947

 

E4-45. Dryden, Hugh L. (1948).

 

E5-5. East Coast Aircraft War Production Council. (1944)

 

E5-10. Educational Institutions - General. 1947-1948.

 

E5-10. [As above. 1941-1947.]

 

E5-10a. Educational Institutions - (Stanford University) 1947-1948.

Box Box 465

E5-10b. Educational Institutions. (Univ of Calif). (1948).

 

E5-10c. Educational Institutions. (Calif. Inst. of Tech.) 1947-1948.

 

E5-10c Seminar re Fluid Mechanics by Prof. K. Stewartson. (CIT) (Univ. of Bristol) at Ames, Dec. 14 & 15, 1953

 

E5-10c. Visit to Jet Propulsion Lab, & Calif Inst of Tech, IAS, & Douglas by Mr. John Spreiter. 2/27 - 29/52.

 

E5-12. Educational Programs - Class Assignments. 1943.

 

E5-12. Educational Programs General. 1941-1947.

 

E5-15. Edwards - General. (1946-1947).

 

E5-20 Engine Res. Lab. (Lewis). 1948.

Box Box 466

As above. Engine Research Lab Cleveland. General. 1944.

 

E5-30. Propellers. (General). [1949]

 

E5-50. Exhibits. (1944-1948).

 

As above. Exhibits. - General. [1941-1947]

Box Box 467

E6-20. NACN. - Motion Picture - General. (1940-1948)

 

E6-30. Films - General. 1953.

 

E6-30. Films - General. 1954

 

E6-30. Films 1949-1959. [Includes U of Cal. Rpt. on Dist of Ames Film.]

Box Box 468

E6-50 Foreign Countries - General. 1954.

 

E6-50 Foreign Countries - General. 1953.

 

E6-50 Foreign Countries. 1942-1953.

Physical Description: [Closed]
 

E6-50 Foreign Countries. England and Canada. (1949-1953).

Box Box 469

E6-50b. France.

 

E6-50b. Foreign Countries - France. 1946-1953.

Physical Description: [Closed]
 

E7-10. Gruman Aircraft Corporation 1944-1947

 

E8-30 Harmond Aircraft Corporation. General. 1943-1944.

 

E7-20. General Electric. 1954.

 

E7-20. General Electric. 1942-1953.

 

E7-20a. G.E. - Upper Atomosphere Rocket Research Panel. 1954.

 

E7-20a General Electric. Upper Atmosphere Rocket Res. Panel. 1950-1953.

 

E7-25. General Motors Corp. 1951-1953.

 

E7-50. Grumman Aircraft. 1954

 

E7-50. Grumman Aircraft Corp. 1949-1953.

Box Box 470

E8-30. Hi. Sp. Flt Station. Gen. 1954.

 

E8-30 Photographic Prints. Also Blueprint Wing Structure D-558 II. 1954.

 

E8-30a Hi High Sp Speed Flt Flight Station. RA Research Authorization 1954

 

E8-30b. Hi Sp Flt Station - Comments. 1954

 

E8-30b. Hi Sp Flt Station - Memos. 1949-1953

Box Box 471

E8-30d. HSFS. Memos. 1954.

 

E8-30d. HSFS. 1949-1953

 

E8-30d. HSFS. Memos. 1950.

 

E8-40. Hiller. 1954.

 

E8-40 and E8-40a Correspondence.

 

E8-50. Hughes. 1954.

 

E8-50. Hughes Aircraft Company. (1948).

 

E8-50. Hughes Aircraft Company. General. 1942-1947.

 

E8-60. Hughes Aircraft. 1951.

 

E8-60. Hughes Aircraft. 1950-53.

 

E9-15. Information - General. 1940-1947

 

E9-20. Inquiries Refered to NACA.

Physical Description: [1 folder]
 

E9-15. Information - General. (1945-1948).

Box Box 472

E9-20. Inquiries Refered to NACA. (1948).

 

Inquiries forwarded to NACA. (1949)

 

E9-30. Roll Stabilization of Free Fall & Rocket Models 1947.

 

E9-40. Helicopters. (1941-1947).

Box Box 473

E9-30. Instruments - General. 1942-1948.

 

E9-40 Instruments - General. 1940-1947.

 

E9-50. Inquires - General. 1954.

 

E9-50. Repts for Gen. Lab. Info. 1949-1953.

 

E9-56. Inquires Ref to NACA. 1952

Physical Description: [2 folders]
 

E9-56. Inquires Ref to NACA. 1950-1953.

Box Box 474

E9-70a. Inspection - Lewis. 1954.

 

E9-70b. Inspection - Lewis. May 5, 7, 13, 1953.

 

E10-5. Joint Research & Development Board (1946-1948).

Box Box 475

E11-1. Langley - General 1954. (1949 & 1951)

 

E11-1. Langley - Gen. 1953.

 

Langley - Gen. 1953.

Box Box 476

E11-1. Langley. 1952.

 

Langley. General. 1954.

 

E11-1. Langley. 1951.

 

E11-1. Langley. 1948.

Box Box 477

E11-1 Langley - General. 1952.

 

E11-1. Langley - General. 1950-1951.

Box Box 478

E11-1a. Langley - Comments. (1953).

Box Box 479

E11-1a. Langley - Comments. (1954)

Box Box 480

E11-1a. Langley - Comments. (1952)

 

E11-1b. Langley Research Authorizations. 1954.

 

E11-1b. Langley RA's. 1951-1953.

Box Box 481

E11-1c. Langley Memos. 1954.

Box Box 482

E11-1c. Langley Memos. 1950-1953.

 

E11-1c. Langley Memos. 1949.

Box Box 483

E11-1d. Langley Paper "Airscoop". 1952-1953.

 

E11-1d. "Airscoop". 1954

 

E11-1c. Weekly Activity Report of the AFDFR at Langley. 1953.

Box Box 484

E11-1e. Langley-Weekly Activity Report of the AFDFR at Langley.

 

E11-1f. Langley - Aircraft Status Reports. 1949-1953.

 

E11-20. Lectures by Ames Staff. 1949-1953.

 

E11-20. Lectures by Ames Staff.

 

E11-21. Lectures by other than Ames. 1949-1954.

 

E11-22. Lewis. (gen). 1950.

Box Box 485

E11-22 Lewis. (gen). 1954.

 

E11-22. Lewis. (gen). 1951.

 

E11-22. Lewis. (gen). 1952.

 

E11-22. Lewis (Gen). 1949.

 

E11-22. Lewis (gen). 1953.

Box Box 486

E11-22a. Lewis - Comments. 1953.

 

E11-22a. Lewis - Comments.

 

E11-22a. Lewis - Comments. 1952.

 

E11-22b. Lewis RA's. 1951-1953.

 

E11-22b. Lewis RAs. 1954.

 

E11-22c. Lewis Memos. 1944-1953.

Box Box 487

E11-22d. Lewis "Orbit" (Formerly Wing Tips) 1954.

 

E11-22d. Lewis Paper:Wing Tips. 1952-1953.

 

E11-30. Library - General. 1940-1953.

 

E11-30. Library - General. 1954.

 

E11-40. Lockheed. 1954.

 

E11-40. Lockheed. 1949-1953

Box Box 488

E12-1. McDonnell. 1946-1953.

 

E12-1. McDonnell a/c Corp. 1952.

 

E12-1. McDonnell Aircraft Corp. 1954.

 

E12-5. Langley Memorial Aeronautical Lab. (1948).

 

E12-5. Langley Aeronautical - Lab. 1940-1947

Box Box 489

E12-5. Langley. (Gen). 1940-1949

 

E12-10. Lectures by Staff Members. (1940-1947).

 

E12-10. Lectures by Ames Staff Members. 1949.

 

E12-10a. Lectures. Speeches etc. by Ames Stall. General. 1944-1949

 

E12-15. Lesley, Evertt P. (1943-1945).

 

E12-15. Marquaedt. 1954.

 

E12-15. Marquaedt. Aircraft Company. 1948-1949

 

E12-17. Lewis. General. 1943-1949.

Box Box 490

E12-20. Martin. 1954.

 

E12-20. Martin. 1954.

 

E12-20. Glenn L. Martin Co. 1949-1953.

 

E12-30. Lockheed Aircraft Corp. (1948)

 

E12-30. Lockheed [and E13-5. McDonnell A/C] 1942-1947.

 

E13-20. National Bureau of Standards. 1949-1953

 

E13-40. Navy - General. 1940-1953

Box Box 491

E13-40. Navy. 1954.

 

E13-40b. Navy - Pt Mugu. 1949-1953.

 

E13-40b. Navy - Point Mugu. 1954.

 

E13-40c. Navy-Naval Ordinance Test Station. 1949-1953

 

E13-40c. Navy - Naval Ordinance Test Installation.

Box Box 492

E13-40d. Navy-Naval Ord. Lab. 1949-1953.

 

E13-40d. [Same title as above.]

 

E13-40e. Navy-Bureau of Economics. 1944-1953.

 

E13-40e. Navy Bu [reau] of Aero [nautics]. 1954

 

E13-40f. Navy NADC. 1954. [NAVY AIR DEVELOPMENT CENTER]

 

E13-40h. Navy NATC [NAVY AIR TEST CENTER]. 1954

Box Box 493

E13-95. North American. 1944-1953.

 

E13-95. North American. [1954]

 

E13-100. Northrop Aircraft. 1944-1953.

 

E13-100. Northrop 1954

 

E14-3. Medicine (Aviation)

Box Box 494

E14-10a. Panels - Res search Airplane Panel 1953-1954

 

E14-10b. Panels-Automatic Control Group. (Goett, Kauffman, and Smith, G.A.) 1953

 

E14-10c. Panels-Computing Machine Panels. 1948-1951

 

As above. 1954

 

E14-10e. Technical Adv isory Panel on Aeronautics. 1954

 

E14-20. Missiles and Rockets. 1949

 

E14-20. Visits to West Coast Guided Missile Contracters, week of 10/5/53, by Niewald of NACA, Goett, Frick, Matthews and Stewart of Ames.

Box Box 495

E14-40. Photographs 1949-1955

Box Box 496

E15-7. Bureau of Standards. 1944-1947

 

E15-7. Bureau of Standards. (1948)

 

E15-8. National Defence Research Council. 1944-1947

 

E15-10. Navy Department-Gen. 1948.

Physical Description: Closed.
 

E15-10. Navy Dept. 1942-1947 Poss Confid.

 

E15-10a. David Taylor Model Basin. (1948)

Physical Description: Closed
Box Box 497

E15-10a. David Taylor Model Basin. (USN) 1944-47.

Physical Description: Closed
 

E15-10b. Navy Dept. - Pilotless Aircraft Unit. (Point Mugu). (1946-1948).

 

E15-10c. Navy Dept. - Naval Ord Test Station - Inyokes. (1945-1948).

 

E15-20. Natl. Research Council of Canada. 1950

 

E15-25c. National Science Foundation. (1947)

Box Box 498

E15-30. National Supersonic Center. Sverdrup and Parcel. 1946-1948

 

E15-40. North American Aviation, Inc. 1944-47

 

E15-40. North American Aviation, Inc. 1948

 

E15-42. North American Aviation, Inc. 1948

Box Box 499

E16-30. Rand Corp. 1954.

 

E16-30. Rand Corp. 1949-1953.

 

E16-50a. Reports in Preparation.

 

E16-50a. Reports - Reports in Preparation. (1950-1953).

Box Box 500

E16-50d. Reports - Requests for in Numbers. 1953-1956.

 

E16-60. Republic. 1948-1953

 

E16-60. Republic. 1954.

Box Box 501

E16-75. Research Programs General. 1940-1954.

Physical Description: 2 folders.
Box Box 502

E16-75. Research Programs. General 1951-1954

 

E16-75. Convertiplane and Engine Proposal. (R. Scheerer) 1949-1952.

Box Box 503

Research - (Ames) Area Rule. 1954-1955.

Physical Description: CLOSED?
 

E16-75. [documents labeled E19-23] Research on External Stores. 592

Box Box 504

E16-75. Bullpup Tests in 6x6 1954-1955. 592

 

E16-75. Review of NACA Static Lateral-Directional Stability Studies. 1953. 592

 

E16-75. Research-Programs-Reversed Pitch Propeller Problem. 592

 

E16-75. Jet-Exit Problems Corres. (Visit by E.A. Mossman) 1950-1954. 592

Box Box 505

E16-75. NACA Program on Supersonic and Transonic Controls (Ames and Langby). 1951-52. 593

 

E16-75. Ribner Triangular Transonic Propeller 593

Box Box 506

E16-75. Jet Engine Research by Ames. (1949-1954) 594

Box Box 507

E16-75. Ryan. 1948-1954. Contains Privilege 595

 

E16-75a. Fire Control. 1952-1955.

 

E17-3b. Panels-Upper Atomsphere Rocket Research Panel (General Electric). (1949).

Box Box 508

E17-10. Photographs (General). 1941-1947

 

E17-10. Photographs - General. (1948).

 

E17-10a. Photographs. AAL Construction Program.

Box Box 509

E17-11. Propellers (General). 1949.

 

E17-11. Part & Whitney. 1945-1950

 

E17-30. Schools and Universities. 1954.

 

E17-30. Schools & Universities. 1949-1953

 

E17-30a. Stanford. 1954.

 

E17-30a. Schools & Universities. Stanford. 1948-1953

 

E17-30b. Schools & Universities. Univ. of California. 1948-1953.

Box Box 510

E17-30b. University of California. 1954.

 

E17-30d. Calif. Inst of Tech. 1954.

 

E17-30d. Schools & Univ. - DIT. 1945-1953.

 

E17-30e. Mass. Inst. of Tech. 1954.

 

E17-30e. Schools & Univ. - MDT. 1949-1953.

 

E17-30h. Schools & Univ. Cornell Univ. 1949-1953.

Box Box 511

E17-31. Comments on University Reports. (1952-1954).

 

E17-60. Societies - General. (1954)

 

E17-60. International Cong. of Mathematicians in Amsterdam, 9/2-9, Attended by W.A. Mersman.

Box Box 512

E17-60. Societies - General. (1951-1953).

 

E17-60. Instrument Society of America Conf. Cleveland - 9/8-12. 1952 attended by Taft Wrathall "Miniature Pressure Cells" paper presented.

Box Box 513

E17-60. Briefing on Analysis of Combat Film by Institute of Air Weapons Research at Univ. of Chicago on 5/19/54 (Attended by G.A. Rathert.)

 

E17-60. American Mathematical Society Meeting - Los Angeles, Nov. 27, 1954

Physical Description: (Two Papers - Martin Shinbrot).
 

E17-60. Photographic Society of America Meeting - Chicago - Week of October 4, 1954 (Attended by John F. Darson).

 

E17-60a. Societies - S.A.E. 1949-1954.

 

E17-60b. Societies - ASME. 1949-1953.

 

E17-60b. Societies - ASME American Society of Machanical Engineers. 1954.

 

E17-60b. Paper by G.A. Smith and W.C. Triplett, "Experimental Flt. Methods for Evaluating Frequency - Response Characteristics of Aircraft" for ASME Meeting in Pittsburg, June 20-24, 1954.

 

E17-60c. Societies - DAS. Institute of Aeronautical Science. 1941-1948.

Box Box 514

E17-60c. Societies - IAS. Institute of Aeronautical Science. 1949-1952.

Box Box 515

As above. 1954.

 

E17-60c. IAS Meeting - Wright Bros Lecture by Dr. Dryden. 1949-1951.

 

E17-60c. Societies - IAS. Inst. of Aeronautical Sciences. 1953.

 

E17-60f. Societies - International Congress of Applied Mechanic. 1950-1953.

Box Box 516

E17-60g. Societies - US National Congress of Applied Mechanic. 1950-1953.

 

E17-60h. Societies - Heat Transfer and Fhird Mechanics Institute.

 

E17-70. Sperry Gyroscope Co. 1953-1954.

 

E17-75. Stanford Research Institute. 1949-1954.

Box Box 517

E19-13. Republic Aviation Corp. 1942-1947.

 

E19-15. Reports. War Time Reports. (Tests of reports copiled and released by NACA on Tech issues). 1946-1949.

Box Box 518

E19-15. (Classif) Reports - Classification Forms. (1947-1950)

 

E19-15 Reports (General) Reproduction. 1947-1948

Box Box 519

E19-15a Reports in Preparation 1951-52

Physical Description: Lists of Pub.
 

E 19-15a Loose Transmittals of Lists of Reports on Tesh. papers in preparation at Ames Lab. 1950-1951

Box Box 520

E19-15a Loose (Some Material as last entry 1946-1950)

Box Box 521

E19-15a Loose (as above 1944-46)

 

E19-15b Reports - Annual Report 1950

 

E19-15b Reports - Annual Reports 1949

Box Box 522

E19-15b Reports - Annual Reports 1946 (as w/327)

 

E19-15b/ Reports - Annual Reports 1948

 

E19-15b. Reports - Annual Reports 1947.

Box Box 523

E19-15b Reports - Annual Reports. 1940-1945

 

E19-15b-1 Annual Bound Bolume Report 1947-1948 Correspondence concerning the above additions, deletions etc

Box Box 524

E19-15b-1 Annual Bound Volume (Jan. - August. 1949) as above

 

E19-15b-1 Annual Bound Bolume (Septs. 1949 - Dec 1950.) as above

Box Box 525

E19-15d;c Loose, as above. 1944-47

 

E19 15d;e;f. Monthly Lists of Preliminary Data, Reports issued by NACA for internal use, and Reports prepared by NACA for AAF. 1943-1947.

Box Box 526

E19-15g;h. Monthly Reports of Aircraft Assigned and Operating at Ames A L. 1946-1949.

 

E19-23. "Application of thin Airfoil Theory to the Study of Cascades." RA proposed by Theo. Aero. Disapproved. 1951.

 

E19-23 Bu Aer Air to Surface Guided Missile Weapon System. 1954. Closed

 

E19-23. Navy Day Fighter Competition. 1952-1953. Closed

 

E19-23 Interceptor - (MX-1554). General - - (Incl Visit by C W Trick to So. Calif Aircraft Companies). 1950-1952 Closed

 

E19-23. (Corres. re visit by Crone and Frick to So. Calif. Industry Plants re Control Surface Problems for Transonic and Supersonic Aircraft. 1950.

 

E19-23. Long Range Interceptor Competition. 1954. Closed

Box Box 527

E19-23. Summary Reports on Experimental Reaearch on Triangular Wings. 1950.

 

E19-23a. Research - General (Study Groups). (1946-1950).

Box Box 528

E19-23 Research, General. 1942-1947

 

E19-23a Summary of Reports on Triangular Wings. 1950

 

E19-24 Request for Authorization on Wind Mills in Transonic Speed Range

Box Box 529

E19-24 Research (NACA Investigations

 

E19-25 Research Program AAL (Test Schedules) AMC Air Material Command Test Schedules. 1943-1947

 

E19-25 Research Program. Ames. General 1942-1947

 

E19-25 AAL Test Schedules. 1942-1950

Box Box 530

E19-25(a) Research Programs. Ames Progress Reports. 1946-1949.

Box Box 531

E19-25a Loose. As above

Box Box 532

E19-25a. Research Program (Progess Reports) 1948-1950.

Box Box 533

E19-15a Loose. As above

Box Box 534

E19-30 Research Reports Comments (LMAL) Tech. Reprots returned from NACA with comments March 26, 1942 - December 31, 1947

Box Box 535

E19-30 Memorandums. General 1941. 26 May thru 1947 December 29, rewvisits, equipment failures, performences

Box Box 536

E19-30 Loose Memorandums & Research Authorizations Jan. 27, 1943-December 11, 1946

Box Box 537

E19-30 Research Authorizations. March 28, 1921 - January 11, 1943

 

E19-30 Preliminary Data - Langley.

Physical Description: empty
Box Box 538

E19-30 As above. 1945-47. Tests of D-558. Douglas 1945 -

Physical Description: 3 folders.
Box Box 539

E19-30 PD's Guided Missiles - JB-2 Flying Bomb; V-1 Flying Bomb; Aeronca Glide Bomb; Interceptor Aircraft. September 22, 1944 - April 11, 1949.

 

EE19-30 (Bell) XS-2 (Army Project 743). 1946.

 

E19-30 P/D Operating Characteristics and Thrust-loading of 2 Six-Blade Dual - Rotating 10 foot Diameter Propellers as Detemined by Wind Tunnel Tests. LMAL. Oct. 8, 1945.

 

E19-30 Memorandums - P-47 B- Republic Aviation. 1942-1943.

Box Box 540

E19-30 P-47B-3 Aileron Study. June 11, 1942.

 

E19-30 P-47D-30 Flying Qualities. 1945.

 

E19-30 P-47C- Flight Tests. March 22, 1944.

 

E19-30 P-47D- Propellers. January 27, 1944

 

E19-30 Memorandums - Bell Co. P-63, P-59 etc. 1943-1944.

 

E19-30 KAQ-1 Ranger/Lark Model Tests Conducted in the Langley Propeller Research Tunnel. June 4, 1946-July 24, 1946.

 

E19-30 Navy "Lark" - High Speed Tunnel. June 4, 1946 - July 24, 1946.

 

E19-30 P-51B General Flight Tests Sept. 29, 1943 - August 19, 1944.

Box Box 541

E19-30 XP-51 - Flight Tests - Compressibility Studies, October 22, 1942 - June 20, 1944

 

E19-30 XP-51F - 19 foot Pressure Tunnel. November 1943.

 

E19-30 XP-51F - Aerodynamic Data - Air - Flow. Research Division. Sept 14, 1943 - October 29, 1943.

 

E19-30 XA-26 - 19-foot Pressure Tunnel. January 4, 1944.

 

E19-30 P-51 - Tests in Full Scale Tunnel. October 27, 1943 - November 5, 1943

 

E19-30 F6F-3 - Flight Tests. March 27, 1944 - August 17, 1944

 

E19-30 XC-82 Horizontal Tail Surface 7 x 10.

 

E19-30 Supersonic Wind-Tunnel Tests and Analysis of a Proposed Supersonic Airplane. 20 Jan 1945.

Box Box 542

E19-30 Effect on Prop. Performance of Tip Modification De Icing Air Flow. July 12, 1944 - August 15, 1944

 

E19-30 XF8B-1- Aerodynamic Data. December 7, 1943 - October 6, 1944.

 

E19-30 P5Y-1 Airplane - Free Flight Tunnel Tests. Janyary 6, 1944.

 

E19-30 A-26B - Flying Qualities. June 6, 1944. September 7, 1944.

 

E19-30 XTB3D-1 (A-26) - Design Information Carburetor Ram Investigation. Wing and Fuselage Combination. August 26, 1943 - Feb 2, 1944

 

E19-30 Power Plant Installation. 1944-1945

Box Box 543

E19-30 XP-77 - Full-Scale Tunnel Tests. January 22, 1944

 

E19-30 P-63 Airplane - Full-Scale Tunnel. November 5, 1943.

 

E19-30 XP-63 - Aileron Effectiveness. April 13, 1942.

 

E19-30 P-63A-1-BE - Flight Tests. 1943-1945

Box Box 544

E19-30 P-38 Airplane - Preliminary Data. March 15, 1942 - March 23, 1943.

 

E19-30 YP-59A - Full Scale Tunnel Tests. 1944.

 

E19-30 "Compressibility Effects MX397 Project. February 15, 1944 - March 20, 1944.

 

E19-30 XBTC-2- Atomospheric Wind Tnnel Tests. 1944.

Box Box 545

 E19-30 As above. 1943-1944.

 

E19-30 Japanese Zero-2 Airplane - Flight Tests. May 27, 1943

 

E19-30 Randome Model - Pressure Distribution. May 10, 1944

 

E19-30 Horizontal Tail Loads Resulting from Landing Impacts. March 15, 1944.

 

E19-30 XP-75 Aileron Development - TDT. September 14, 1944 - October 26, 1943.

 

E19-30 XP-75 Aileron Development - Flight Tests. May 15, 1944 - July 15, 1944.

 

E19-30 Constriction Effects in High Speed Wind Tunnels. January 31, 1944.

 

E19-30 NACA 7-11-12, 8-H-12, 9-H-12 and 10-H-12 Airfoils Sections - Aerodynamic Data, February 29, 1944

Box Box 546

E19-30 RA-30 Airplane - Flight Investigation of Sideslip Characteristics. January 26, 1944

 

E19-30 Aileron Control - NACA Studies. June 28, 1943.

 

E19-30 XF2M-1 - General Motors Model, November 17, 1943.

 

E19-30 YR-4A Helicopter - Aerodynamic Data. March 29, 1944

 

E19-30 XBTM-1 - Aerodynamic Data

 

E19-30 XBTM-1 - Free-Spinning Tunnel Tests of 1/20 - Scale Model. August 10, 1945.

 

E19-30 XB-36 Nacelle. February 9, 1944 - April 30, 1945.

 

E19-30 B-36 Powered Model - 19 foot Model. 1944-1945.

Box Box 547

E19-30 XF-12 Direct Coupled Gyroscope - Langley Roll Stabilization System. 1944-1948.

Box Box 548

E19-30 XF-12. 1945-1946

Box Box 549

E19-30 NACA 23015 and NACA 16-212 Airfoils. XB-35 Elevon Model at High Speeds. December 16, 1942 - January 26, 1945.

 

E19-30 XB-35-Elevon Development. Drag Data. Propeller Characterstics

Physical Description: empty
Box Box 550

E19-30 XB-42 - Tail Propeller Interference Tests. G-17 Airfoil Duct Model. MX-392. February 18, 1944 - September 12, 1944.

Box Box 551

E19-30 PD - "LMAL Full Scale Tests of the Grumman XF8F-1 Airplane - - Part 1 - Drag Tests." January 13, 1945 - December 20, 1946

 

E19-30 XP-67 - Wing Inlet and Duct Designs. October 14, 1943.

 

E19-30 XP-72 Model - Atmospheric Wind Tunnel. August 5, 1944-Septermber 4, 1944.

 

E19-30 XB-39 - Full Scale Tunnel. Engine Nacelle. June 17, 1944.

 

E19-30 XP-69 - Compressibility Effects. Feb. 22, 1943

 

E19-30 Performance Selection of 3000 HP Pursuits Airplanes. February 26, 1944.

 

E19-30 B-33 - Balacned Ailerons. Frise Aileron. Feb 27, 1942 - April 13, 1942.

 

E19-30 B-32-19 Foot Tunnel. Low Turbulence Section. May 10, 1944 - July 27, 1944

Box Box 552

E19-30 P-40 K. Tail Loads Investigation. July 28, 1943 - February 21, 1944.

Box Box 553

E19-30. P-40 K. Tail Loads Investigation. April 5, 1944 - November 8, 1944

 

E19-30 F4F-3- Flap Tests on Semispan Model. April 18, 1944.

 

E19-30 SB2D-1- Tests in LMAL 16 - foot Tunnel. August 22, 1944.

 

E19-30 XP-60- Preliminary Data from 19-Foot Pressur Tunnel. May 9, 1941.

 

E19-30 JRM-1 Model - Wind Tunnel. September 4, 1944.

 

E19-30 Douglas C-74 - Aerodynamic Data. November 7, 1944 - December 13, 1944.

 

E19-30 NACA 66, 2-216 and NACA 66 (215) - 216 Airfoils - Aerodymanic Data. November 5, 1943 - January 19, 1944.

 

E19-30 JRM-1 Model - Wind Tunnel. September 4, 1944.

 

E19-30 Douglas C-74 - Aerodynamic Data. November 7, 1944 - December 13, 1944.

 

E19-30 NACA 66, 2-216 and NACA 66 (215) - 216 Airfoils - Aerodynamic Data. November 5, 1943 - January 19, 1944.

 

E19-30 CNAC 1/35 - Scale Tailless Airplane, Free-flight Tunnel Tests. August 15, 1944.

 

E19-30 65, 3-018 Wing Section - TDT. Sept. 29, 1942.

 

E19-30 XP-84 - Inv. of Aerodynamic Characteristics of Lefthand Horizontal Tail Surface in 16 T. Part II

Physical Description: [empty]
 

E19-30 MX-578 Republic. Investigation in 16 of Lefthand Horizontal Tail Surface. Parts I - III. May 28, 1945 - June 5, 1945

 

E19-30 P-80A (MX-596) - Free-Flight Tunnel Tail Tests. June 15, 1945.

 

E19-30 XF5U-1 - Tests 1/3 - Scale Model in Full Scale Tunnel. June 8 - Aug 4, 1945

 

E19-30 XF6U-1 - Aerodynamic Data. May 19 - August 6, 1945.

 

E19-30 XB-43 (MX-475) Aerodynamic Data. July 3-5, 1945.

 

E19-30 XTB3F-1. P/D - Tests of 1/8 Scale Model. October 5, 1945 - February 27, 1946.

 

E19-30 P/D Wind Tunnel Tests of the 1/4.5 Scale Model of the Bell L-39-1 Airplane. June 4, 1946 - Sept. 19, 1946.

Box Box 554

E19-30 Tests of JB-2 Air Logs in Langley 16-foot High - Speed Tunnel. July 30, 1945.

 

E19-30 Tests of Seven Types of Impellers for the JB-2 Air Logs in the Langley 16 foot High Speed Tunnel. Sept. 4, 1945.

 

E19-30 P/D Investigation of Icing Characteristics of a PBM-3D Cooling - Fan Installation AERL, Cleveland Co. April 23, 1946.

 

E19-30 Langley P/D "Wind Tunnel Tests of Army Project MX-578 XXII - Pressur Distribution Over Fuselage Nose, Original Canopy, and V-Front Canopy." October 11, 1945

Box Box 555

E19-30 Langley P.D "Free-Spinning Tunnel Tests of a 1/20 - Scale Model of the Curtiss-Wright XF15C-1 Airplane II - Spin Recover Parachute Requirements TED No. NACA 2366. October 4 - November 27, 1945

 

E19-30 Langley Paper: "Multichannel Pressure Transmitter for Measuring Pressures on a Rotating Propeller," by Arthur A. Reiger. November 20, 1945.

 

E19-30 P/D Development of Tip Nozzles for Heated - Air Anti-Icing Propellers. Part I - Description of Equipment. July 6, 1945

 

E19-30 P/D Basic Thickness Forms for the NACA 651-006, 651-009, 651-010, 661-006 and 661-009 Airfoil Sections. December 18, 1944.

 

E19-30 Allison V-3420-11 Engine - - Ground Tests at the Full-Scale Tunnel. August 16, 1944

 

E19-30 P.D. "Ordinates ofr the NACA-1408, 1410, 1412, 641-110, and 641-112. Airfoil Sections. November 3, 1944.

 

E19-30 PD-"Wing-Tunnel Tests of a Swept-Back Wing, Chordwise Pressure Distribution and Spanwise Normal - Force Loading" January 23 - January 29, 1945.

 

E19-30 Tailess Pusher Airplane - Free - Flight Tunnel Tests. September 18, 1943 - December 8, 1944.

 

E19-30 P/D 1/7 Scale Model of the Kaiser Tailess Airplane Part I - Lift and Drag Measurements. May 9, 1945.

 

E19-30 XF-15C-1 Aerodynamic Data for Airfoil Section Equipped With Double-Slotted Flap for Curtiss-Wright XF-15C-1 Airplane II Lift and Pitching-Moment Data; etc. July 7, 1944.

 

E19-30 Guided Missiles - Free Flight Tunnel. May 22 - August 6, 1945.

 

E19-30 PD High Speed WT Tests of an Experimental AS-27 Antenna Model No. 1 with 45° Sweepback. Aug. 4, 1945.

Box Box 556

E19-30 P/D Negative - Thrust Tests of Single - and Dual - Rotating Tractor Props. August 31, 1943.

 

E19-30 Memo For Files: "A Preliminary Trial of a Pressure Belt," by Blake Corson. Aug. 12, 1942.

 

E19-30 Memo for Files "Tests Made in a One Inch Nozzle to Compare Aerody Data Obtained in an Atomosphere of FREON 12 with that obtained in Air." by Von Doenhoeff and Braslon. April 4, 1947

 

E19-30 CMR "Propeller and Cooling - Air - Flow char. of Twin Engine Airplane Model..." by McHug and Pepper

Physical Description: (empty)
 

E19-30 P/D Two Dimensional Wind - Tunnel Investigation at High Reynolds nos. of two Symetrical Circular - Arc Airfoil Sections with High Lift Devices LMAL July 3, 1944.

 

E19-30 Langley Paper: "Multichannel Pressure Transmitter for Measuring Pressures on a Rotating Propeller," by Arthur A. Reiger, 11/20/45.

 

E19-30 LMAL "Low-Speed Tests of 5 NACA 66-Series Airfoils Hairing Mean Lines Designed to Give High Critical Mach Numbers," by von Doenhoff, Stivers Je., O'Conner. April 11, 1946

 

E19-30 (Comments). (1947-48).

 

E19-30 LMAL Memo - "Measurements of the Motions of Shock Waves" by J.W. Benson. (1947).

 

E19-30 (Memos.) (1948).

Box Box 557

E19-30 Research Program. Aircraft Loads Division. Apr. - Aug. 1950 Apr. - Aug. 1950

 

E19-30. Comments. 1951.

Box Box 558

E19-30 Comments. 1950.

 

E19-30. Comments. 1949

 

E19-30. Comments. 1949-1951.

Box Box 559

E19-30 Langley (Research. General) 1940-1949.

 

E19-30. (Memos) Langley Memo. 1949.

Box Box 560

E19-30. Langley-Progress of Papers. 1951-1952

 

E19-30. Langley-Progress of Papers. 1950-1951

Box Box 561

E19-30. Research Program - Aircraft Loads Division. 1950-1951

Box Box 562

E19-30. General 1951.

Box Box 563

E19-30. Research Program. Aircraft Loads Division. Jan. - Apr. 1950.

Box Box 564

E19-30 MR "The Problem of Noise Reduction With Reference to Light Airplanes" by T. Theodorsen and Arthur A. Regier.

 

E19-30 Langley Rpt. "Effect of Shark Design on Propeller Performance at High Speeds," by J.B. Delan and M.M. Carmel - 12/29/45

 

E19-30 Memo for Files - "A Pressure Transfer Device for Measure Simultaneously 24 Pressures on Rotating Airfoils" by Miller and Habel dated May 28, 1946.

 

E19-30 P/D. I. 4/14/45 Autom. Pilot Charac.

 

P/D. II. 4/14/45 Lat. Char. of Orig. Design

 

P/D. III. 4/25/45 Lat. Char. with inc. tail Gargoyle LBD-1 area

 

E19-33 General. Drawings Flight 12-13X4#2

 

E19-35 Research Program (AERL) Lewis Flight Propulsion Lab. 1943-1947.

Box Box 565

E19-35 Research Reports Comments (Cleveland) Lewis Flight Propulsion Lab. June 7, 1945 - December 2, 1947.

 

E19-35 Lewis - Research Authorizations. 1943-1950

 

E19-35 Preliminary Data - General. March 23, 1945.

 

E19-35 "Velocity Distributions on Arbitrary Airfoils in Closed Tunnels by Conformal Mapping.

 

E19-35 P-80 Transcontinental Speed Record Report and Analysis of Fuel Consumptions made by Cleveland Lab Staff. 1946.

 

E19-35 Pro. (posed) Adv. (anced) Restr. (ricted) Report "A Method of Matching the Performance of Compressor Systems With that of Aircraft Power Sections." Keetch & Moses - October, 1945 - February 7, 1946.

 

E19-35 CR "Relaxation Calculations of the Effects of Compressibility on the Two-Dimensional Wind Tunnel Constriction Correction for Subsonic Flows: Epstein, Brinich, Albers, December 1945

 

E19-35 AERL RPT. "A Constant - Gain Crystal Knock Pickup Amplifier" by Richard P. Krebs and Thomas Dallas (AERL-November 1945) (R.A. E-19)

 

E19-35 Pro [posed] Adv. [anced] Restr. [icted] Report" Experimental Investigation of the Jet-Boundary Constriction Correction for a Model Spanning a Closed Cir cular Tunnel. November 1945.

 

E19-35 (General). (1948)

 

E19-35 (Comments). (1948)

 

E19-35 ACR "The Jet-Boundry Constriction Correction for Summetrical Airfoils in a Closed Tunnel, etc. W. Perl and H.E. Moses, dated 11/45.

Box Box 565

E19-35 ACR "The Jet - Boundary Constriction Correction for Symmetrical Airfoils in a Closed Tunnel, etc. W. Perl and H.E. Moses, 11/45.

Box Box 566

E19-35 YP-59A - Power-Plant Installation 1944.

Box Box 567

E19-35 P/D Altitude - Wind-Tunnel Tests of Westinghouse 19B and 19XB Engines. 1944-1945

 

E19-35 Prosp. ACR "The Minimum Pressure Attainable on an Airfoil in Mixed Supersonic Flow, by W. Perl (AERL - March, 1946)

 

E19-35 Paper: An Optical Method of Angular Demagnification with Application to a Recording Inclinometer. February 23, 1945.

 

E19-35 P/D "Icing Char. of Bendix-Stromberg PT-13G-1 Carburetor Mounted on Pratt Whitney R-2800-51 Accessory Housing Assembly. July 7, 1945.

 

E19-35 P/D "Flame Damping of Turbosuper - charger Installation by Mears of Exhaust-Gas Heat Exchanger: April 15, 1944

 

E19-35 P/Analysis "Comparison of the Performance Charac. of the Westinghouse Sup-Stage Axial-Flow Compressors Models 19-B and 9. 5a dated July 11, 1945.

 

E19-35 B-26B- Temperature Distribution on a R-2800-5 engine. Oct. 5, 1943 - March 22, 1944.

Box Box 568

E19-35 P/D "Perf. Tests of G.E. I-16 J-P Unit Equipped with Ryan XFR-1 Cowling. Ducting and Tailpipe. October 1944.

 

E19-35 Alcohl De-Icing Tests of the C-46 Induction System Part II, Altitude Air-Box Tests of Four Alcohol, De-Icing Systems conducted at Cleveland. June 1, 1945 Part II

 

E19-35 Memo "Spiral Shielded Thermocouple for Measuring Exhaust - Gas Temperatures" Harmon May 18, 1944.

 

E19-35 P/D "Performance Tests of G.E. Type I-A Supercharger, Unit 10". February 22, 1944.

 

E19-35 P/D "Icing Char. of Special Aircraft Antennas." December 14, 1944.

 

E19-35 Report "Electronic Indicator for Angular Velocity and Acceleration." by Krebs. May - June 1944.

 

E19-35 P/ARR "Two-Dimensional Incompressible Potential Flow Over Corrugated and Distorted Surfaces." by Mutterperl and Green. June - July 1944.

 

E19-35 P/D "Performance Tests of G.E. Type I-A Supercharger, Unit 10". February 22, 1944.

 

E19-35 P/D "Icing Char. of Special Aircraft Antennas." December 14, 1944.

 

E19-35 Report "Electronic Indicator for Angular Velocity and Acceleration." by Drebs. May - June 1944

 

E19-35 P/ARR "Two-Dimensional Incompressible Potential Flow Over Corrugated and Distorted Surfaces." by Mutterperl and Green. June - July 1944.

 

E19-35 CMR "Flame Visibility Tests with Individual Exhaust Stack" by Turner and Humble March 19, 1943.

 

E19-35 ARR - "Engine Tests of Pressurized Shunt Type Cooling Systems for a Liquid-Cooled Engine. January 1944

 

E19-35 P/D "Altitude-Wind Tunnel Tests of the Locheed YP-80a Power-Plant Installation - Part I," dated April 30, 1945.

Box Box 569

E19-35 As above. Loose March - August 1945.

Box Box 570

E19-35 P/D "Two NACA Fuel-Injection Modifications that Prevent Serious Refrigeration Icing in the Induction System of Allison V-1710-89. April 17, 1945.

 

E19-35 Calculation of Thrust of a Compressor Combustion - Turbine Jet Propulsion Engine. AERL. July 11, 1944.

 

E19-35 "A Method for Remote Indication of Propeller-Pitch Angle" and "Ratio-Meter Type of Propeller-Pitch Indicator" by Warshaw. May 15, 1945.

 

E19-35 P/D Development of Protected Carburetor - air scoop for Induction System of C-46 airplane dated May 19, 1945.

 

E19-35 RMR "A Multiple Bridge for Elimination of Contract-Resistance Errors in Resistance Strain-Gage Measurements, Warshwasky. June, 1945.

 

E19-35 "Meteorlogical Summary of Conditions Observed During NACA Icing Tests at Cleveland, Ohio. During Winter of 1946-1947" by Dwight B. Kline.

 

E19-36 (Comments). (1948).

 

E19-36 Research, General. Contracts w/Schools. 1943-1947

 

E19-36 (General). (1940-1948).

 

E19-36 (Copies of Research Contracts with Schools). (1943-48).

Box Box 571

E19-36 Comments. 1949-1951. Stanford Univ. - Contract W535 - ac - 18162 dtd. Feb. 10, 1941. "Report on Flutter." (AAF).

Box Box 572

Stanford Univ. - NA w-5322 -

Physical Description: High Intensity Lamps.
 

Stanford Univ. - NA w-2946.

Physical Description: Propeller Plan.
 

Stanford Univ. - NA w-5469.

Physical Description: High Intensity Lamps.
 

Univ. of California. - NA w-5459.

Physical Description: Waterdrop Trajectories.
 

E19-40. United Aircraft. 1950-1954.

 

E-45 Ryan Aeronautical General Correspondence 1943-1946

Box Box 573

E19-60 Scientific Research Board (Presidents). (1946-1947).

 

E20-20 Socities-General.

 

E20-11 Stack, John. 1946

 

E20-20. Heat Trans and Fluid Mech Inst. (1949).

 

E20-20. Societies - General. (1948).

Box Box 574

E20-20a. Societies - SAE. (1940-1948).

 

E20-20b. Societies - ASME. (1946-1948).

Box Box 575

E20-20c. As above.

 

E20-20e. Societies - Aircraft Industries Assoc. ARYC on Flutter Research, 1948-1949

 

E20-20e. Prelim. Corres. re Wright Bros Lecture by Dr. Dryden under S,A,S, (1949).

Box Boxes 576-581

Closed

Box Box 582

E20-25q. Visits - Reports by Ames Staff. 1940-1954

Box Box 583

E21-10. Tests - Weekly Schedules of Tests. 1943-1947.

 

E21-10. Westinghouse. 1952-1954

 

E21-30. Enclosures to Langley. 3-1-50. 1950

 

E22-20. United Arilines - General. (1944-1948).

 

E23-3. Vega Aircraft. 1942-1943

 

E23-10. All Corres. re MX-1179. (1950-1952).

Box Box 584

E23-10a. Reports of Visits to Ames. 1940-1949.

 

E23-106. British - Visit to England by Fred Mattheson - September, 1953.

 

E23-20b. Visit of Dr. A.C. Charters to Navy Ord Lab, Harvard College Observatory and Ballistic Research Lab, Aberdeen Pro. Gr, Oct. 26 - Nov. 4., 1953.

 

E23-20b. Visits by Charles W. Frick to England and France (9/29/52 - 11/27/52)

Physical Description: Possibly Close?
 

E23-10b. Visit to Various Aircraft Companies in L.A. to Discuss Fiberglass Reinforced Plastic Techniques (Betts - Elam and Pahle). Nov., 1953.

Box Box 585

E24-5- Status of Investigations for the AAF at Ames Lab. 1952.

 

E24-5- Progress Reports of AAF Projects Investigated at Ames. 1950-1951.

Box Box 586

E24-5. War Dept - Arny Liaison Office. 1943

Box Box 587

E24-5. War Dept - Army Liaison Office 1942-1946.

 

E24-5. War Dept - Liaison Info. 1943-1945.

 

E24-20. Warner, Dr. Edward P. (1942-1944).

Box Box 588

Equipment EMC Equipment Branch. 1950-1954

Box Box 589

G3-20. Chambers of Commerce. 1939-1948.

 

G3-25a. Quart Reports of Franked Mail. Admin. Div. 1940-1946

 

G3-25d. Mail - Delays, etc. Adm. Services. (1940-1949).

 

G3-30. Construction Projects - General. 1940 thru 1947.

Box Box 590

G7-40. Drawings from Mare Island Naval Shipyard re Torpedo Tube Firing Mechanism. March 14, 1948.

Physical Description: Closed
Box Box 591

G7-40c. N.A.S. Moffett Field.

 

G5-30. Equipment (Microsyn). (1949).

 

G5-30a. OPA Mileage Report.

 

G5-30b. Annual Motor Vehicles Rpts. 1943-1948

 

G5-34. Property. July 1942 - Aug. 1948.

 

G12-5k. Laboratory - Visits to (Group Tours, Open house, etc.) 1945-1949

Box Box 592

G12-6. Labor - General.

 

G12-6b. Labor - Wage Rate Determination

 

G12-6c. Labor - Wages.

Box Box 593

G15-10- National Defense - General.

 

G15-10a. National Defense - Blackout Regulations.

 

G15-10b. National Defense - Camouflage.

 

G15-10c National Defense - National Defense Sec Against Sabotage

 

G20-3. Safety Commitee. 1951-1954.

 

G21-18. Tire Rationing.

 

G21-18 Monthly Report of Papers for Office of War Information.

Box Box 594

Miscellaneous Correspondence from R.A.'s. 1946-1949

 

R.A. A-41 XFR-1 Airplane. Ryan. 1945.

 

R.A. A-45 Investigation of "Rumbling" of North American XP-51B Airplan. 1948.

 

R.A. A-58 Investigation of Dougle-Hinged Control for the Horizontal Tail of an Airplane 1954

 

R.A. A-160 High-Speed Wind Tunnel Invest. of NACA66 (215)-210 Airfoil with Modified Mean Comber Line. 1946

 

R.A. A-161 Study of Bodies Suitable for Supersonic Flight. 1946-1951.

 

R.A. A-166 Lockheed P-80 Project MX409 (1945)

 

R.A. A-173. Investigation to Determine Optimum Configurations for Jet and Turbine Driven Airplanes 1946-1948

 

R.A. A-174. "High Speed Wind Tunnel Investigation of Consolidated Vultee Lark". 1945-1948

 

R.A. A-175. Investigation of Flying Qualities of Chance-Vought F4U-4 Airplane. 1947

 

R.A. A-178. Determination of Wing Structure Temperatures During High-Speed Flight Maneuvers. 1950

Box Box 595

R.A. A-181. Study of Dynamic Stability and Control of Airplanes. (Flt. Res.) 1945-1954.

 

R.A. A-183. Investigation of the Flying Qualities of a Lockheed P-80A. 1945-1951.

 

R.A. A-186 Full-Scale Research on Boundary Layer Control for Swept Wings. 1950

 

R.A. A-192. Inv. of Fluctuating Pressures on Wings at Transonic Speeds. 1946-1947

 

R.A. A193. Investigation of Characteristics of Wings at High Reynolds Num. and High Subsonic Mach Numbers. 1946-1947.

Box Box 596

R.A. A194 Wind Tunnel Tests of Project MX-656 1948-1950

Box Box 597

R.A. A-194 Investigation of Aero. Characteristics of Ducts and Ducts and Duct Inlets Suitable for Supersonic Flight. 1948-1949

 

R.A. A-196. Investigation of Aerodynamic Characteristics of Ryan XF22-2 Airplane. 1947

 

R.A. A-197 Investigation of Stat. and Control Character of Full-Scale Model of Republic XP-91 Airplane. 1948-1949

 

R.A. A-199. Full-Scale Invest. of Effects of Airplane Density on Oscillatory Divergence of Airplane with Sweptback Wing. 1946-1951.

Box Box 598

RA A-199 F86 Drawings. 1951 (also check 1028-1029)

Box Box 599

RA. A-208. Investigations of Full-Scale Empennage of Boeing XB-47. Airplane in 40 X 80 W/T. AAF. 1946-1947

 

R.A. A-208 Drawings. B.T2D-1 Aircraft. 1948

Box Box 600

R.A. A-210. Investigation of Full-Scale Characteristics of Consolidate Vultee XP-92 in 40 x 80. 1946-1951.

 

R.A. A-211. 40 x 80 Foot Wind Tunnel Inv. of McDonnell XP-85 Airplane. AAF (R). 1947-1948.

 

R.A. A-213. Hi-Speed W.T. Inv of Compressibility Problems of Typical Twin Inlet Turbo - Jet Fighter Aircraft. (BuAer). (C). 1945-1950.

 

R.A. A-214. Fundamental Study of Leading Edge Air Inlets on Swept Wings. (Subcomm. on Inter Flow.) (C.).

 

R.A. A215. Inv of High-Frequency Undamped Oscillations of High-Speed Airplanes. (C) (Subcomm. on Stab. and Cont.). 1945-1948.

 

R.A. A217 7 x 10 W.T. Inv. of Rep. XP-91 Airplane to Compare Conventional and Vee-Tail Arrangements. (C). 1947-1950.

Physical Description: (AAF). 7 x 10.
Box Box 601

R.A. A218.- Wing Tunnel Invest. on XS-3 Research Airplane. (C) 16 (AAF) (MX656). 1947-1955

 

R.A. 219 Surface Temp. and Heat Transfer to Bodies at Supersonic Speeds. 1947-1948.

Box Box 602

R.A. 218. (Drawings). 1956

Box Boxes 603, 604, 605

RA 218 - Wind Tunnel Tests of Project MX656. 1948-1950

Box Box 606

R.A. A-220 Fundamental Inv of Boundary - Layer Phenomena in Compressible Flow, Effs. Heat Trans. 1947-1950.

 

R.A. A-221. Inv of Boundary Layer Control to Obtain Reductions in Drag at Sub and Super Speeds. 1947-1948.

 

R.A. A-222 Inv of Downwash and Wake of Wings at Supersonic Speeds. 1948.

 

R.A. A-223. High-Speed Wind-Tunnel Tests of Fairchild Model XSAM-2 (Lark) Pilotless Aircraft. 1947-1952.

Physical Description: 16
 

R.A. A-224. Invest of Effects of Sweep, Low Aspect Ratio, and Thin Wing Sec on Stalling char. of Airplanes. 1947-1951.

Box Box 606

R.A. A-220. Fundamental Inv of Boundary - Layer Phenomena in Compressible Flow. Effs. Heat Trans. 1947-1950.

 

R.A. A-221. Inv of Boundary Layer Control to Obtain Reductions in Drag at Sub and Super Speeds. 1947-1948.

 

R.A. A-222. Inv of Downwash and Wake of Wings at Supersonic Speeds. 1948.

 

R.A. A-223. High-Speed Wind-Tunnel Tests of Fairchild Model XSAM-2 (Lark) Pilotless Aircraft. 1947-1952.

Physical Description: 16.
 

R.A. A-224. Invest of Effects of Sweep, Low Aspect Ratio, and Thin Wing Sec on Stalling har. of Airplanes. 1947-1951.

 

RA A-225 Investigation of Aerodynamic Maneuvering Brakes for High Speed Aircraft. 1947.

Box Box 607

R.A. A-226 Supersonic Wind - Tunnel Inv. of Lockheed Ram-Jet Test Vehicle. 1947-1954

Physical Description: 1 x 3.
 

R.A. A-227 Invest of Effects of Wing Inter. and Closeness of Resonce upon First-order Vibration Stresses of Prop. Blades. 1948-1950

Physical Description: 40 x 80.
 

R.A. A-228 High Speed Studies of Prop. Spinner - Cooling Configuration. (S.C Propellers for Aircraft). 1948-1949.

Box Box 608

R.A. A-230 Theoretical Research on Stability Derivatives for Transonic and Supersonic Flight. 1948.

 

R.A. A-231. Invest. of Mutual Interf. Between Intersecting Airfoils and Between Arifoils and Bodies. 1948.

 

R.A. A-232. Aerodynamic Effects of Jets and Jet Exits. 1947-1949.

 

R.A. A-233. Invest of High Speed Aerody. Characteristics of Martin XB-51 Bomber. 1947-1948.

 

R.A. A-235 W/T Invest. of Horizontal-Vertical Tail Surface Interaction on McDonnell XF2H-1 Airplane. 1948-1949.

Physical Description: 16
 

R.A. A-236 Exper. Invest. of Stability Derivatives of H/S Aircraft and Component Parts. Confidential. S/C Stability and Control.

 

R.A. A-236 March and April. 1950.

Box Box 609

R.A. A-237 Invest. of Characteristics of Control Surfaces at Transonic and Supersonic Speeds. Confid. 1948-1950.

 

R.A. A-238 Invest. of Atability and Control Character of Grumman XSSM-6 Pilotless Aircraft. Confid. Buero. 1949-1951.

 

R.A. A-240 Invest, of Radio Cont. for Obt. Aero Data on Full-Scle in Flight at High Mach Number. 1947-1951.

 

R.A. A-241. Tests of a Cross-Wind Landing Gear. 1948.

Box  Box 610, 611

R.A. A242. Drawings Only. 1946

Box Box 612

R.A. A-242. Tests to Determine Loads on F-84 Wing Due to Tip Tanks and Aero-Elastic Effects. 1948-1950

 

R.A. A-244 Inv. Bon-Wave Detachment from Airfoil Sections at Low Supersonic Spds. Confed. 1950-1951.

Physical Description: 1 x 3.
 

R.A. A-246 "Study of Aeroelastic Effects on Aircraft Suitable for High Speed Flight." (C). 1947-1950.

 

R.A. A-247 "Inv. of Aero. Charact. of 1/16 - Scale Model of Bumblebee Prototype Test Vehicle. 16." (C). 1949.

 

R.A. A-250. "Wind Tunnel Invest. of Aeroelastic Eff. on Stab. of Northrop MX-775 Missile. AAF. C. 1950.

Physical Description: 40 x 80.
 

R.A. A-251. Supersonic Wind-Tunnel Invest. of Aerodynamic Characteristics of Douglas XF4D-1 Airplane. 1949-1951.

Box Box 613

R.A. A-252 Supersonic Wind Tunnel Investigation of Boeing GAPA Model 601. (MX-606). 1945-1950

 

R.A. A-253 Inv. of Airplane Shaking at Stall and at Supercritical Mach Numbers. (c) FR-16 - 1x3½ - 40x80. S/C Hi - Sp. 1949-1950

 

493 - R.A. A254 Drawings 1950

 

R.A. A-254. "W/T Inv. of Aerodynamic Char. of x-3 Research Airplane At Supersonic Speeds." 1950.

Physical Description: (5) 6-by6- Ft W/T. AMC.
 

1123 - R.A. A254. Wind Tunnel Tests of ProjectMX 656 1948-1950

Box Box 614

R.A. A-255. Flt. Invest. of Control Motion and Manuevering Tail Loads on Large Air-Planes. Flt. Rea. S/C Aircraft Loads (R). R60-1 (Constituation). 1949-1952.

Box Box 615

R.A. A-256. High Spd. WT Invest. of Aerodynamic Char of Boeing XB-52 (MX-839) Airplane (C) 16. AMC.

 

1130. R.A. A-256. (MX-839). XB-52. (1949)

 

S21-75. (R.A. A-256). XB-52. MX-839 Preliminary Correspondence. Boeing 1950

 

493. RA257. Drawings. 1949

Box Box 616

R.A. A-257. Supersonic Wind-Tunnel Tests of the Sperry XAAM-N-2. (Sparrow) Pilotless Aircraft. (C). 1948-1951.

 

494. RA261 Drawings 1950

Box Box 617

R.A. A-258. "High Speed Wind-Tunnel Investi of Horizontal Tail of Northrop F-89 Airplane. (C). 1950-1951

 

R.A. A-259. Wind-Tunnel Test of Air Sampling Devices. (C). (Chemical Corps. Dept. of Army). 1950.

 

R.A. A-260. Investigation of Wing-Tails Interference of MX-904 Guided Missile. (C). 1951

Physical Description: 1x3.
 

R.A. A-261. Supersonic Wind-Tunnel Investigation of MX-775A. (C). 1950-1951

Physical Description: 6x6.
 

R.A. A-262. "Inv. Effects Non Linearities on the Dynamic Response of Aircraft (Unclass) S/C Stab. and Con. 1950

 

Records of the Ames Unitary Plan Design Group, 1950-1953

Box Box 1

Lewis. C-NAW-6002 to 6220. 1952-1954.

 

Lewis. NA3-1831 to 2449. 1952-1954.

Box Box 2

L - and NA1 - Contracts. 1953-1956

 

Langley - Requisitions and Contracts.

Box Box 3

Ames - Requisitions and Contracts. 1950-1954

 

Lewis Orders. C - Bids.

 

Lewis - Condition of Appropriation. 1953-1954.

Box Box 4

Lewis - Cost Estimate, Fiscal Programming.

Box Box 5

Langley - Condition of Appropriation, Monthly Fiscal Reports. 1951-1955.

 

Lewis - Requisitions and Contracts. 1952-1956.

 

Ames - Project and Modifications Approval. 1950-53.

Box Box 6

Loose Papers. Fiscal Budget 1955-56.

 

Langley - Cost Estimate, Fiscal Programming. 1950-1954.

Box Box 7

Supersonic Facility Unit. Organization and Personnel. 1948-1949.

 

Unitary Plan - Ames. 1953-54.

Physical Description: Good photo of W/T Construction.
Box Box 8

Lewis - Project and Modification Approvals. 1950-1956.

 

Langley - Project and Modification Approvals. 1950-1956.

 

Langley - Miscellaneous Correspondence. 1950-1955.

 

Unitary Plan Progress Reports - 1954. also 1955-56

 

Lewis - Miscellaneous Correspondence. 1950-1954.

Box Box 9

Unitary Plan - Budget Submittals. 1950-1953.

 

Unitary Plan - Memos for Files - 1950.

 

Unitary Plan - Memos for Files - 1951 -1954

Box Box 10

Unitary Plan - Progress Reports. 1950-1954.

 

As above. 1950-54

Box Box 11

Ames - Miscellaneous Correspondence.

Box Box 12

Loose Paper. Unitary Plan. 1950-1954.

Box Box 13

Instrumentation Unitary Plan. 1949-1954.

Physical Description: General Correspondence.
Box Box 14

Unitary. - Langley Drawings.

Physical Description: Blueprints
Box Box 15

Specifications. #'s C-3418 to C-3485. Unitary Plan

Physical Description: [17 folders]
Box Box 16

Specifications. #'s C-3489 - C3975 Unitary Plan.

Physical Description: [23folders]
 

Specifications 1948-1955

Box Box 17

Lewis. Specifications C-361 - C-3416. Lewis -

Physical Description: [20folders]
Box Box 18

Specifications C-4048 - C-4495. Lewis -

Physical Description: 23 [folders]
Box Box 19

Specifications. Lewis Standard General Building Specs. C-4093 - C-4940.

Physical Description: 16 folders.
Box Box 20

Specifications. C-4423 - C-4439.

Physical Description: [9 folders]
Box Box 21

Specifications. C-4444 - C-5019.

Physical Description: [20 folders]
Box Box 22

Specifications. C-5026 - C-5513.

Physical Description: [17 folders]
Box Box 23

Specifications. L-4556 - L-5978.

Physical Description: [25 folders]
Box Box 24

Specifications. L-6957 - L-7768

Physical Description: [6 folders]
Box Box 25

Specifications. L-5928 - L-7507

Physical Description: [15 folders]
Box Box 26

C D 109900. - C D 109970. Blueprints. Unitary Plan 1952.

Box Box 27

C D 109970 - C D 110041. Blueprints. Unitary Plan 1952.

Box Box 28

C D - 111 ---; C D S -: C E - 108 ---; Blueprints; Unitary Plan

Box Box 29

CE - 111200; CES-: CR; Misc; Blueprints 1952.

Physical Description: [4 folders]
Box Box 30

Specifications. C-4433. Blueprint 1952 Unitary Plan

 

CAS - 100 --. Blueprint. 1952

Box Box 31

C B - Blueprint. 1952

 

C D - 106 - Blueprint. 1952

 

C D - 107650 Blueprint. 1952

Box Box 32

C D - 107700 Blueprint. 1952

Box Box 33

C D - 107750 Blueprint. 1952

 

C D - 108 Blueprint. 1952

Box Box 34

C D 108399 - C D 108462. Blueprint. 1952.

Box Box 35

C D 110165 - Blueprints & Drawings. 54.

Box Box 36

EE - 16890 - EE - 16896 Blueprints 52.

 

EE 17566 - EE - 17873 Blueprints

Box Box 37

CE - 109462 - CE - 109424. 1952.

Box Box 38

C D - 106911 - C D 110292. 1952.

 

CE - 109301 - CD109469. Blueprints. 52.

Box Box 39

Loose. CE - 109317 - CE1093833 Blueprints. 52.

Box Box 40

Loose. CE - 109384 - 109424 Blueprints. 52.

Box Box 41

CL - 6020R - CD5 - 1413 Drawings. 1951.

 

Loose Blueprints. 1945-46. Axial Flow Compressor.

Box Box 42

Loose Blueprints Axial Flow Compressor 1947.

 

Cleveland.

Physical Description: 6x8-ft Tunnel Compressor Drawings.
 

Loose Drawings and Blueprints Compressor. 48.

Box Box 43

Loose Blueprints and Drawings. 1948-1950.

 

16 foot Wind. 1953.

Physical Description: Blueprints.
Box Box 44

EE - 17902 - EE - 17912. Blueprints. 1946-1947.

 

J2769. Drawings. Unitary Wind Tunnel.

Box Box 45

CE - 111114 to CE 109383. Loose Drawings. 1952.

 

ED - 17570 - ED - 17850. Blueprints. 1946-47.

Physical Description: 8x6 SSWT
 

8 - Foot Transonic Wind Tunnel. Drawings. 1946.

Box Box 46

J2769. Loose Drawings. 1947-1948.

 

Misc Langley Drawings - Props and Spinners; Survey Equip; Cowlings. Photostats of Turbine Specs. 1944-1947.

Physical Description: [4 folders]
Box Box 47

EEP12369-G LFPL 16" and 24" Explosion Relief Valves. Drawings. 1942-43.

 

CE81718 LFPL 8 Differential Manometer Board. Drawing 1950.

 

ERL Wind Tunnel. 1941. [work papers]

Physical Description: 13 folders.
Box Box 48

As above. 1941 [Workpapers]

Physical Description: 21 folders.
Box Box 49

As above. 1941-42. [Workpapers]

Physical Description: 10 folders.
Box Box 50

As above. 1942. [Workpapers]

Physical Description: 10 folders.
Box Box 51

As above. 1941-42. [Workpapers]

Physical Description: 17 folders.
 

LE - 46850. Blueprints 1951. Unitary Plots.

Box Box 52

ES - 5812. Blueprints 1951 Unitary Plan

 

LD - 42301 Blueprints 1951 Unitary Plan

 

LD - 46848 Blueprints 1951 Unitary Plan

Box Box 53

LD - 46851. Blueprints. Unitary Plan. 1951.

 

LD - 46861. Blueprints. Unitary Plan. 1951.

 

LD - 46866. Blueprints. Unitary Plan. 1952.

 

LD - 46860. Blueprints. Unitary Plan. 1951.

Box Box 54

LD - 46866. Blueprints. Unitary Plan. 1952

 

LD - 46870. Blueprints. Unitary Plan. 1952

Box Box 55

LD - 46874 Blueprints. Unitary Plan. 1952

 

LD - 46875 Blueprints. Unitary Plan. 1952

 

LD - 46876 Blueprints. Unitary Plan. 1952

Box Box 56

218870 - Blueprints. Unitary Plan. 1952.

 

L - 6564 Blueprints. Unitary Plan. 1953.

Box Box 57

Spec. L - 6639. Strain Gage Indicators. Blueprints. Unitary Plan. 1953.

 

LD - 46877 Blueprints. 1953.

Box Box 58

LD - 46877. Blueprints. 1952. Unitary Plan.

 

LD - 46878. Blueprints. 1952. Unitary Plan.

Box Box 59

LD - 46878. Blueprints. 1952. Unitary Plan.

Box Box 60

LD - 46879. Blueprints. 1952. Unitary Plan.

 

LX - 46890. Blueprints. 1952. Unitary.

Box Box 61

LX - 46890. Blueprints. Unitary Plan. 1951-52.

 

LE - 46891. Blueprints. Unitary Plan. 1951-52.

Box Box 62

LD - 46892. Blueprints. Unitary Plan. 1951-52.

 

LD - 46893. Blueprints. Unitary Plan. 1951.

 

LD - 46894. Blueprints. Unitary Plan. 1952.

 

LD - 46895. Blueprints. Unitary Plan. 1952.

 

LD - 72081. Blueprints. Unitary Plan. 1951.

 

LD - 72081. Blueprints. Unitary Plan. 1951.

Box Box 63

LD - 76041. Blueprints. Unitary Plan. 1951-52.

 

LD - 76043. Blueprints. Unitary Plan. 1951.

 

21 - 9001E - 21 - 9072. Blueprints. Unitary Plan. 1951-52.

Box Box 64

Unitary - General Corres. 1954.

 

U - 2. Unitary - Corres re Brochure. 1954.

 

U1 - 10. Authorization of Unitary Plan and Hearing Statements before the Comm on Armed Service (House of Rep. 1949).

 

U3 5. Classification (Unitary Plan). 1952.

 

U4 - 5. Unitary Design - General. 1948 - 1955.

Physical Description: CLOSED
Box Box 65

[Loose Drawings] Unitary Plan Wind Tunnel 1946-1954.

Box Box 66

As above.

Box Box 67

As above.

Box Box 68

As above.

 

Records of the Research Instrumentation Division, 1941-1956

Box Box 1

Instrument Development - General. 1950-1954

Box Box 2

Instrument - General. 1948-1954.

Box Box 3

Inst. Dev. - Accelerometer Units. 1948-1956.

 

Inst. Dev. - Altimeters. 1947-1953.

 

Inst. Dev. - Cathetometers. 1949-1953.

 

Inst. Dev. - Dew Point Meters. 1945-1952.

 

Inst. Dev. - Diaphrams. 1949-1950.

 

Inst. Dev. - Film Drums. 1947-1951.

 

Inst. Dev. - Film Reader - (Telereader). 1946-1952.

 

Inst. Dev. - Galvanometers. 1949-1953.

 

Inst. Dev. - Gyroscopes. 1954.

 

Inst. Dev. - Indicator, Angle of Attack. 1949-1954.

 

Inst. Dev. - Indicator, Mixture. 1947-1952.

Box Box 4

Inst. Dev. - Manometers (General). 1948-1955.

Box Box 5

Inst. Dev. - Manometers (micromanometers). 1940-1954.

 

Inst. Dev. - Pressure Gages. 1949-1954

 

Inst. Dev. - Potentiometers. 1950-1953.

 

Inst. Dev. - Radar Beacons. 1950.

 

Inst. Dev. - Recorder. Rainbow (Cloud-Meter). 1950-1951.

 

Inst. Dev. - Recorders - VG. 1943-1955.

 

Inst. Dev. - Recorder - Stick Force. 1942.

 

Inst. Dev. - Recorder. Miniature Sequence. 1951.

Box Box 6

Inst. Dev. - Recorders - Flight. 1947-1954.

 

Instrument Dev. - Recorder, Magnetic Tape Data. 1954-1955.

 

Instrument Dev. - Recorders - 1954-1955. Miniature Temperature.

 

Inst. Dev. Splined Couplings. 1941

 

Inst. Dev. Selector Switches 1942

 

Inst. Dev. - Thermometer. Electrical Resistance 1946-1948

 

Inst. Dev. - Thermometer, Calibration of 1946-1948

 

Inst. Dev. - Timers - Tuning Fork. 1949-1956.

 

Inst. Dev. - Turnometers. 1945-1946.

 

Inst. Dev. - Vibration Testing Table (Oscellating). 1949-1953.

 

Inst. Dev. - Wake Survey Machine. 1941.

 

Report Unit Files, 1947-1954

Box Box 1

TN-1391 by William Lewis. 1947-1950

 

TN-1791 by Holdaway. 1948-1949.

 

RM A9C09. by Jones and Lewis. 1948-1949.

 

TN-1904 by Lew & Hoecker. 1949.

 

TN 1855 by Jones and Lewis. 1948-1950.

 

TN 2212 by Neel and Bright. 1950-1951.

 

"A Probability Analysis of the Meteorlogical Factors Conductive to Aircraft Icing" by W. Lewis. 1950-1951. No Number

 

RM A51H15. by White and Look. 1951

 

TN 2476 by Bergun. 1951

 

TN 2615 by Neel and Steinmetz. 1951-1952.

 

TN 2738 by Lewis and Bergrun. 1951-1953

Box Box 1A

Spreiter. AL-47. Theo Aero. RM A51L17. Original Text. Positives. 1951

 

MN Mead. AG-38. GRM A51K05. O.T.P. 1951

Physical Description: 6x6.
 

S. Sherman Edwards. AG-29. CRM A51J19 OTP etc.

Physical Description: 6x6.
 

Frank A. Pfyl. AG-36. CRM A51I18. OTP etc

Physical Description: 6x6.
 

John C Heitmeyer. AG-39. CRM A51H22. O.T.P. etc

Physical Description: 6x6.
 

John C Heitmeyer. AG-37. CRM A51H10. O.T.P. etc

Physical Description: 6x6.
 

John C Heitmeyer. AG-35. CRM A51H02. O.T.P. etc

Physical Description: 6x6.
 

AG-30. CRM A51F12. O.T.P. 1951

Physical Description: 6x6.
 

Hall and Heitmeyer. AG-32. CRM A51E01. O.T.P. etc

Physical Description: 6x6.
 

RM A51 H20 (A-3-1 A4) and CRM A51 B14. Selna

Box Box 2

Ray Phelps and Frank Lazzeroni. RM A51E28. AG-31. OTPND

 

John C. Heitmeyer. CRM A51D30. AG-33. OTPN.D

 

John C. Heitmeyer. and Romald Hightower. AG-34. CRM A51F21. OTPND

Physical Description: 6x6.
 

John W. Boyd. AG-20. CRM A51C13. O.T.P.N.D.

Physical Description: 6x6.
 

Benton E. Wetzel and Frank AG_@@. CRM A51B20. O.T.P.N.D.

Physical Description: 6x6.
 

Wyss and Sorenson. AB-34. CRM A51J10. O.T.P.N.D.

Physical Description: 16-Foot.
 

J. F. Strond. AE-57. CRM A51K14. O.T.P.N.D.

Physical Description: 1x3.
 

RM A52F27. By John Selna, L.G. Bright. B.A. Schlaff.

Box Box 3

Ben Johnson and Harry Shibarta, AF-24. CRM A51D27. O.T.P.N.D.

 

Elliot Katzen and Geo. Kaatari. AE-45. CRM A51C27. O.T.P.N.D.

Physical Description: 1x3.
 

Spahr and Robinson. RM A51C08. AE-37. O.T.P.N.D.

Physical Description: 1x3.
 

Scherrer and Dennis. AE-38. CRM A51A03. O.T.P.N.D.

Physical Description: 1x3.
 

John Stroud and Warren Anderson. AE-49. CRM A51A09. OTPND

Physical Description: 1x3.
 

Leonard M. Rose. AA-52. CRM A51D25. OTPND

Physical Description: 7x10.
Box Box 4

Earl C. Watson. CRM A51F15. OTPND

Physical Description: 7x10.
 

Edward Hopkins and Hurbert C. Cerel. AA-51. CRM A51G24. O.T.P.N.D.

Physical Description: 7x10.
 

Matthews and McNeill. Flt. Res. AN-55. OTPND

 

Grahm and Koenig. AD-44. RM A51L013. OTPND

Physical Description: 40x80.
 

Cook and Kelly. AD-45. RM A51J24. OTPND

Physical Description: 40x80.
 

Howard Matthews and Edward Stuart. Flt. Res. AN-31. CRM A51F18. OTPND

 

Smith, Shibata, and Selon. AF-32. CRM A51K28. O.T.P.N.D.

Physical Description: 12-Foot.
Box Box 5

Boddy, Lee. F. And Emerson, Horace. F. O.F.N.D. RM A9J20.

Physical Description: 16-foot Tunnel.
 

Smith and Reed. 12 foot. AF-29. CRM A51L21 O.T.P.N.D.

Physical Description: 4 folders
 

Robert H. Barnes. AB-41. RM A51I25. O.T.P.N.D.

Physical Description: 16 foot.
 

Stephanson and Selon. 12-foot. AF-28. CRM A51Io7. O.T.P.N.D.

Physical Description: 2 folders
Box Box 6

Reynolds and Sammonds. AF-19. RM A51E03. O.T.P.N.D.

Physical Description: 12-Foot.
 

Kolbe and Baudettine. AF-21. RM A51D02. OTPND

Physical Description: 12-foot.
 

Kolbe and Baltz. 12 foot. AF-27. RM A51G31. O.T.P.N.D.

Physical Description: 4 folders
Box Box 7

Burnett L. Gadeburg. Flt Res. AN-51. TN 2525. O.T.P.N.D.

 

Marvin Shinbrat. Flt Res. AH-26. TN 2341. O.T.P.N.D.

 

Harvey H. Brown. AA-37. TN 2490. O.T.P.N.D.

Physical Description: 2 folders
 

Liddell, Creer and Van Dyck. Flt Res. AH-39. RM A51E16. OTPND

 

Seth B. Anderson. Flt Res. AH-25. CRM A51E14. OTPND

 

Anderson, Ernst and Van Dyck. Flt Res. AH-38. CRM A51B28. O.T.P.N.D.

 

Neel and Sternmetz. Flt Engr. AK-22. TN 2615. OTPND

 

Stalder and Zurick. Flt Engr. AK-19. TN 2423. OTPND

Box Box 8

Bergrun. TN 2416. Flt Eng. AK-15. OTPND

Physical Description: 3 folders
 

Triplett and Smith. Flt Res. AH-41. CRM A51G27. OTPND

 

White and Look. Flt Eng. AK-24. CRM A51H15. OTPND

 

Selna and Schlaff. Flt Eng. AK-26. RM A51H20. OTPND

Box Box 9

Morris W. Rubesin. Flt Eng. AK-20. TN 2345. O.T.P.N.D.

 

Higgins and Pappas. Flt Eng. AK-18. TN 2351. O.T.P.N.D.

 

James Selna. Flt Eng. AK-17. CRM A51B14. O.T.P.N.D.

 

Muroc. Sadoff, Ankenbruck, and O'Hare. CRM A51H09. AM-2. O.T.P.N.D.

 

Grahm and Koenig. AD-46. RM A51H10A. O.T.P.N.D.

Physical Description: 40x80.
 

Grahm and Koenig. RM A51B21. AA-43. O.T.P.N.D.

Physical Description: 40x80.
 

James Drew. RM A51D18. OTPND

Physical Description: 40x80.
 

Paul Yaggy. AD-47. TN 2528. OTPND

Physical Description: 40x80.
 

Rogallo, Roberts & Oldaker. AD-37. TN 2308. OTPND

Physical Description: 40x80.
Box Box 10

Ralph L. Maki. AD-42. RM A51E15 OTPND

Physical Description: 40x80.
 

Smaus, Gore, Waugh. Inst. Dev. AM-6. TN 2578. OTPND

 

Smaus and Stewart. Inst. Dev. AM-7. Tn 2373. OTPND

 

McDevitt. AB-45. RM A51L17b. OTPND

Physical Description: 16-foot.
 

Robert A. Taylor. AB-42. RM A51L03a. OTPND

Physical Description: 16-foot.
 

Cleary & Stevens. AB-43. CRM A51J11. OTPND

Physical Description: 16-foot.
 

Frank and Taylor. AB-38. CRM A51H20a. OTPND

Physical Description: 16-foot.
 

Stalder, Goodwin and Creager. Flt. Eng. AK-21. Proposed TN 2428. OTPND

Box Box 11

Vernon J Rossow. SSFF. AO-4. Proposed TN 2399. OTPFND

 

Edwin C. Allen. 16. CRM A51F12a. AB-39. OTPFND

 

Sacks. AL-40. Theo. Aero. TN 2605. OTPND

 

Fuller and Briggs. Theo Aero. AL-37. Tn 2335. OTPFND

 

Lomax & Byrd. AL-33. TN 2554 OTPND

 

Lomax & Heaslet. Theo Aero. AL-36. TN 2497. OTPND

 

Sacks and Spreiter. Theo Aero. AL-26. TN 2323. OTPND

 

Altman and Hayter. AA-49. TN-2500 OTPFND

Physical Description: 7x10.
Box Box 12

Mc Cullough and Gault. AA-50. TN 2502. OTPFND

Physical Description: 7x10.
 

Holzhauser. AA-54. CRM A51J19A. OTPFND

Physical Description: 7x10.
 

Kelly and Hayter. AA-53. CRM A51H23. OTPFND

Physical Description: 7x10.
 

Morris D. Friedman. Theo Aero AL-38. RM A51I20. OTPFND

 

Lomax, Neaslet, and Studer. Theo Aero. TN 2403. AL-34. OTPFND

 

Lomax, Neaslet, and Studer. Theo Aero. TN 2387. AL-22. OTPFND

Box Box 13

Blackaby. AA-45. TN 2379. OTPND

Physical Description: 7x10.
 

Dannenberg. AA-41. RM A51E29 OTPFND

Physical Description: 7x10.
 

Holzhouser. AA-48. CRM A51E24. OTPND

Physical Description: 7x10.
 

Delany and Hayter. AA-39. RM A51A16. OTPND

Physical Description: 7x10.
 

Perkins, Gowen and Jergensen. AE-40. CRM 51G13. OTPFND

Physical Description: 1x3.
 

Vincenti and Waggoner. AE-51. TN 2588. OTPND

Physical Description: 1x3.
 

Chapman, Wimbrow and Kester. AE-59. TN 2611. OTPND

 

Spahr and Dickey. AE-46. Proposed TN 2360. OTPFND

Physical Description: 1x3.
 

Milton Van Dyke. TN 2670. AC 27. O.T.N.D.

Physical Description: 1x3½.
Box Box 14

As above

 

Laurence, Schmedt and Loaschen. AC-26. TN 2509. OTPND

Physical Description: 1x3½.
 

Walker, Stivers and Beard. AC-25. CRM A51B16. OTPFND

Physical Description: 1x3½foot.
 

High Speed Research. AG-59. TN 2919. OTPFND

 

Hamaker, Niece and Evans. TN 2443. AN-3. OTPFND

Physical Description: 10x14.
 

Hamaker and Wong. AN-4. TN 2631. OTPFND

Physical Description: 10x14.
 

Eggers and Smith. AN-6. TN 2579. OTPFND

Physical Description: 10x14.
 

Edward Hopkins. AA-46. CRM A51C14. OTPFND

Physical Description: 7x10.
Box Box 15

TN 3347. AF-65.

Physical Description: 12-Foot.
 

TN 3348. AG-75.

Physical Description: 6x6.
 

TN 3224. AG-64.

Physical Description: 6x6.
 

TN 3386. AG-72.

Physical Description: 6x6.
 

TN 3130. AK 35. Flt Engr.

Box Box 16

Edwards, Tinling and Ackerman. RM A52F18.

 

Bruce E. Tinling. RM A52119.

 

NACA RM A52K20. AF-40.

Physical Description: 12-Foot,
 

RM A52I19a. AF-38.

 

CRM A52D01a.

Physical Description: 12-Foot.
 

CRM A52G07.

Physical Description: 12 Foot
 

CRM A52G02. AF-35.

Physical Description: 12-Foot
Box Box 17

RM SA52E06. AF-39.

Physical Description: 12-Foot.
 

RRM A52D22.

Physical Description: 12-Foot
 

CRM A52D01.

Physical Description: 12-Foot.
 

CRM A52B20.

Physical Description: 12-Foot.
 

RM A52130.

Physical Description: 1x3.
 

RM A52D29.

Box Box 18

A52H28.

Physical Description: 1x3.
 

RM A52D17.

Physical Description: 1x3
 

AD-68. CRM A52C20.

Physical Description: 1x3 Foot.
 

CRM A52F17.

Physical Description: 1x3
 

CRM A52B06. AE-66.

Physical Description: 1x3.
 

NACA RM A52E27. SSFR. AH-57

 

RM A52I23. AH-61.

 

RM A52J06. AH-60. Flt. Res.

 

RM A52A31. AH-47. Flt. Res.

 

Flt. Res. RM A52A14.

 

984. RM 52F16.

 

RM A52A04.

Box Box 19

CRM SA52L31. AH-68. Flt. Res.

 

RM A52L16a.

 

RM A52J22. Flt Res.

Box Box 20

AF-31. CRM A52B20. O.T. 1952

Physical Description: 12-foot.
 

Accession 57A254 1952 AF-68. RM A52E06. O.T.P. 1952

Physical Description: 12-foot.
 

AF-34. RM A52D01. O.T. 1952

Physical Description: 12-foot.
Box Box 21

AF-35. RM A52G02. O.T.P. 1952

Physical Description: 12-foot.
 

AF-36. CRM A52F18. O.T.P. 1952

Physical Description: 12-foot.
 

AF-42. CRM A52I19. O.T.P. 1952

Physical Description: 12-foot.
 

AF-41. CRM A52G07. O.T.P. 1952

Physical Description: 12-foot.
Box Box 22

AF-30. RRM A52D22. O.T.P. 1952

Physical Description: 12-foot. [2 Folders]
Box Box 23

AB-52. RM A52D11. O.T.P. 1952

Physical Description: 16-foot.
 

SSFF. AO-1. Conf. RM A52A24. O.T.P. 1952

 

SSFF. AO-2. RRM A52A14B. O.T.P. 1952

Box Box 24

SSFF. AO-5. RM A52C24. O.T.P. 1952

 

SSFF. AO-9. TN 2764. O.T. 1952

 

Theo Aero. AL-21. TN 2825, O.T.P. 1952

 

Theo. Aero. AL-46. TN 2744. O.T.P. 1952

 

Theo. Aero. AL-41. TN 2707. O.T.P. 1952

Box Box 25

12 Foot. AF-40. RM A52K20. O.T. 1952

Physical Description: [2 Folders]
Box Box 26

Flt Research. RM A52LI6a. O.T.P. 1952

 

AD-62. RM A52LI6. O.T.P. 1952

Physical Description: 40x80.
 

16. RM A52J17. O.T.P. 1952

 

16. AB-51. RM A52J21. O.T.P. 1952

 

Flt Res. AH-58. RMAA52I17. O.T.P. 1952

 

Flt Res. AH-42. TN 2820. O.T.P. 1952

Box Box 27

Flt Res. AH-62. TN 2877 O.T.P. 1952

 

Flt Res. AH-56. CRM A52AO4. O.T.P. 1952

 

Flt. Res. AN-65. RM A52K12. O.T.P. 1952

 

Flt. Res. AN-35. TN 2622. O.T.P. 1952

 

AN-14. TN 2811. O.T.P. 1952

Physical Description: 10x14.
 

AN-14. TN 2646. O.T.P. 1952

Physical Description: 10x14.
 

AN-10. TN 2729. O.T.P. 1952

Physical Description: 10x14.
 

AN-18. TN 2922. O.T.P. 1952

Physical Description: 10x14.
 

AN-17. TN 2690. O.T.P. 1952

Physical Description: 10x14.
Box Box 28

AE-62. TN 2664. O.T.P. 1952

Physical Description: 10x14.
 

AE-68. TN 2960. O.T.P. 1952

Physical Description: 10x14.
 

AE-67. RM A52F17. O.T.P. 1952

Physical Description: 10x14.
Box Box 29

AM-4. TN 2845. O.T.P. 1952

Physical Description: 10x14.
 

AD-50. RM A52JO8. O.T.P. 1952

Physical Description: 40x80.
 

AD-49. RM A52BO5. O.T.P. 1952

Physical Description: 40x80.
 

AD-53. RM A52B19 O.T.P. 1952

Physical Description: 40x80.
Physical Description: [2 folders]
Box Box 30

AD-63. TN 2894. O.T.P.N.D.

Physical Description: 40x80.
 

I.D. AD-48. TN 3008 O.T.P.N.D.

Physical Description: 40x80.
 

AD-57. TN 2795. O.T.P.N.D.

Physical Description: 40x80.
 

AD-61. RM A52L15. O.T.P. 1952

Physical Description: 40x80.
 

AD-55. RM A52K13. O.T.P. 1952

Physical Description: 40x80.
 

AP-1. TN 2686. O.T.P.N.D.

Physical Description: 40x80.
Box Box 31

7x10. AA-56. RM A52A17. O.T.P. 1952

Physical Description: 2 folders
 

7x10. AA-60. RM A52DO16. O.T.P. 1952

 

Flt Eng. AK-23. TN 2738. O.T.P. N.D.

 

7x10. AA-55. A52C14. O.T.P. 1952

Box Box 32

Flt Eng. AK-28. RM A52F16. O.T.P. 1952

 

Flt. Eng. AK-29. RN 2852. O.T.P. N.D.

 

Flt. Res. AH-68. CRM SA52L31. O.T.P. 1952

 

AA-58. RM A52F13. O.T.P. 1952

Physical Description: 7x10.
 

AD-59. SA52HO4. O.T.P. 1952

Physical Description: 40x80.
 

LD and HT. AP-2. TN 2740. O.T.P.N.D.

 

AD-58. CRM SA52D25. O.T.P. 1952

Physical Description: 40x80.
 

AD-3. TN. HEAT TRANSFER O.T.P. 1952

 

AD-52. RM A52A14A. O.T.P. 1952

Physical Description: 40x80.
Box Box 33

AG-57. RM A52LO4. O.T.P. 1952

Physical Description: 6x6. [3 envelopes]
Box Box 34

AG-56. CRM A52K14. O.T.P. 1952

Physical Description: 6x6.
 

AG-55. RM A52LO2. O.T.P. 1952

Physical Description: 6x6.
 

AG-50. CRM A52L15a. O.T.P. 1952

Physical Description: 6x6.
 

Flt Res. AH-48. CRM A52A14. O.T.P. 1952

 

Flt Res. AH-57. CRM A52E27. O.T.P. 1952

 

Flt Res. AH-61. CRM A52I23. O.T.P. 1952

Box Box 35

Flt Res. AH-60. CRM A52JO6. O.T.P. 1952

 

Flt Res. AH-59. CRM A52J22. O.T.P. 1952

 

AE-76. CRM A52I30. O.T.P. 1952

Physical Description: 1x3.
 

AA-57 TN 2847. O.T.P. 1952

Physical Description: 7x10.
Box Box 36

AG-41. CRM A52DO1c. O.T.P. 1952

Physical Description: 6x6.
 

AG-44. CRM A52C04. O.T.P. 1952

Physical Description: 6x6.
 

AG-40. CRM A52B08. O.T.P. 1952

Physical Description: 6x6.
 

AG-46. CRM A52C10a. O.T.P. 1952

Physical Description: 6x6.
 

AG-45. CRM A52D23. O.T.P. 1952

Physical Description: 6x6.
Box Box 37

AG-42. CRM A52E01. O.T.P. 1952

Physical Description: 6x6.
 

AG-51. CRM A52J 31. O.T.P. 1952

Physical Description: 6x6.
 

AG-48. CRM A52J30. O.T.P. 1952

Physical Description: 6x6.
 

AG-52. CRM A52 G29. O.T.P. 1952

Physical Description: 6x6.
 

AG-47. SA52E07. O.T.P. 1952

Physical Description: 6x6.
Box Box 38

AN-13. CRM A52K07. O.T.P. 1952

Physical Description: 10x14.
 

AB-49. CRM A52D21. O.T.P. 1952

Physical Description: 16 Tunnel.
 

AB-44. CRM A52C07. O.T.P. 1952

Physical Description: 16 Tunnel.
 

TR1088 (formerly TN 2270.) O.T.P. N.D.

Physical Description: 6x6.
 

AG-54. CRM A52L04a. O.T.P. 1952

Physical Description: 6x6.
 

TECH. REPORT 1188. TOBAK. Original Figures Only. A-8.

 

RM A52G17 (Now TR1276). 1952.

Physical Description: 40x80.
 

RM A52A18. AM-5. O.T.P. 1952

Box Box 39

TN 3223. AQ-1. Unitary

 

RM A52K 12. Flt Res.

 

TN ____. AH-62. Flt Res.

 

TN 2845. AM-4. 10x14 and Inst. Dev.

 

A-2-2 A28-3. TN. 1952

 

CRM A52G17. AD-56.

Physical Description: 40x80.
Box Box 40

RM SA52J15. 40x80 and Inst Dev. J.O. 2949.

 

RM SA52H04. Hunlon, Griffin and James.

 

Restricted RM A52B19.

Physical Description: 40x80.
 

RM SA52D25.

Physical Description: 40x80.
 

David G. Koenig. RM A52L15.

Physical Description: 40x80
 

RRM A52B05. Maki. AD-49

Physical Description: 40x80.
 

NACA RM A52K13.

Physical Description: 40x80.
 

NACA RM 52A14a.

Physical Description: 40x80.
 

RM A52A10. AD-48.

Physical Description: 40x80.
 

Franks. RM A52L16.

Physical Description: 40x80
 

Nelson and Krunm. AB-52. A52D11.

Physical Description: 16 Foot.
 

Martin and Reed. RM A52E05.

Physical Description: 16 Foot.
 

RM A52J21. AB-51.

Physical Description: 16 Foot.
 

RM A52J17. Martin and Reed.

Physical Description: 16 Foot.
 

Emerson and Gale. NACA Conf. RM A52C07.

Physical Description: 16WT.
Box Box 41

RM A52D21. AB-49.

Physical Description: 16.
 

John C Hertmeyer. RM A52L15a.

 

Willard G. Smith. AG-48.

Physical Description: 6x6.
 

RM A52L04a. AG-54.

Physical Description: 6x6.
 

RM A52629. AG-52

Physical Description: 6x6.
 

RM A52E23.

Physical Description: 6x6.
 

RM A52E07.

Physical Description: 6x6.
 

NACA RM A52D23.

 

RM A52D01c. AC-41.

Physical Description: 6x6.
 

RM A52C10a.

Physical Description: 6x6.
 

RM A52C04.

Physical Description: 6x6.
 

NACA RM A52B08. SSWT.

Physical Description: 6x6.
Box Box 42

RM A52L04. AG-57.

Physical Description: 6x6.
 

AG-55. RM A52L02.

 

NACA RM A52K14.

Physical Description: 6x6.
 

RM A52F27. AK-30

 

NACA RM A52F16. A9-5.

 

A52C24. SSFF. AD-5.

 

RM A52B13. SSFF.

 

RM A52A14B. SSFF.

 

CRM SA52C10. SSFF.

 

SSFF. RRM A52A24.

 

RM A52A24. AN-11.

Physical Description: 10x14.
Box Box 43

RM A5E20.

 

RM A52E22.

Physical Description: 10x14.
 

RM A52K07. AN-13.

Physical Description: 10x14.
 

CRM A52F13.

Physical Description: 7x10.
 

A52A17. AA-56.

Physical Description: 7x10.
 

RM A52D01B.

Physical Description: 7x10.
 

RM A52A18. AM-5. Instrument Development.

 

AH-64. CRM A53G10. Flt Res.

 

RM A53H12. Flt Res.

 

CRM A53H10. AH-74. Flight Res.

 

CRM A53G22. AH-73. Flt Res.

Box Box 44

TN 3285. AA-67.

Physical Description: 7x10.
 

TN 3220. AA-68.

Physical Description: 7x10.
 

3170. AA-66.

Physical Description: 7x10.
 

RM 53A514.

Physical Description: 7x10.
 

TN 3007. AA-63.

Physical Description: 7x10.
 

TN 3138.

Physical Description: 7x10.
 

TN 3093. AA-64.

Physical Description: 7x10.
 

Unclass TN. J02479-R-1.

Physical Description: 7x10.
 

AA-65. TN 3094.

Physical Description: 7x10.
 

TN 2847. J.0. 2649R.

Physical Description: 7x10.
 

TN 3226. AE-103.

Physical Description: 1x3.
 

TN. 1486R1.

Physical Description: 1x3.
Box Box 45

TN 2832. AE-73.

 

J.0. 1892R2. Unclassified TN.

Physical Description: 1x3 ft.
 

AE-91. TN 3097.

Physical Description: 1x3.
 

AE-69. RM A53E01.

Physical Description: 1x3.
 

TN 3225. AE-92.

Physical Description: 6x6 and 1x3.
 

TN 3499. AE-107.

Physical Description: 1x3.
 

J.0. 2823.R. TN ____. SSFF

 

TN 3391. AO-17. SSFF

 

TN 3284. AO-15. SSFF

 

TN 3125. AO-14. SSFF

 

TN 3095. AD-22.

Physical Description: 10x14.
 

A.J. Eggers Jr. AN-14. TN 2811.

 

TN 2694. AN-15.

Physical Description: 10x14.
 

TN 2927. Syvertson and Savin.

 

John A. Axelson. CRM A53123.

Physical Description: 16 foot.
Box Box 46

CRM A53129.

Physical Description: 16 ft.
 

TN 3036.

Physical Description: 16 ft.
 

TN 3129. AB-54.

Physical Description: 16 ft.
 

AC-35. TN 3127.

Physical Description: 1x3-½.
 

AC-30. TN 2998.

Physical Description: 1x3-½.
 

AC-31. TN 3162

Physical Description: 1x3-½.
 

A-7-1 A47-1. AC-33.

Physical Description: 1x3½
 

TN 3087. AC-34

Physical Description: 1x3½.
 

RM A53E29. AC-28.

Physical Description: 1x3½.
 

AP-4. TN 3222. LDHT.

 

AP-2. 2740. J02583-R.

 

TN, Unclass. J0 2700R. Heat Transfer.

 

Rogallo and McCloud. AD-65.

Physical Description: 40x80.
 

Lynn W. Hunton and Harry A. Jones. AD-67. TN 3840.

Physical Description: 40x80.
 

TN by Vernon L Rogallo. AD-57.

Physical Description: 40x80.
 

TN 2894. Vernon L. Rogallo and John L. McCloud. AD-63.

Physical Description: 40x80.
 

Lynn W. Hunton. AD-48. TN 3008.

Physical Description: 40x80.
 

Wick, Bradford H. TN 3221. AD-74 CRM A53I01. Hi-Speed-Unitary.

Physical Description: 40x80.
Box Box 47

CRM A53F23. Flt Res.

 

RM A53E21. Flt Res.

 

RM A53A15. Flt. Res.

Physical Description: 40x80.
 

AH-67. Flt Res. CRM A53B11.

 

RM A53A06. Flt Res.

 

AK -33. RM A53H17. Flt Eng.

 

Conf. RM 53816 - Flt Eng.

 

TN 2852. Flt Eng. 1918 -R.

 

TN 3025. Flt Eng.

 

TN 2985. AK-31. Flt. Engr.

 

CRM A53E06. AD-64.

Physical Description: 40x80.
Box Box 48

AD-66. A53D21.

Physical Description: 40x80.
 

RM A53D14.

Physical Description: 40x80.
 

AD-69. CRM A53J26.

Physical Description: 40x80.
 

AA-59. RM A53H03.

Physical Description: 7x10.
 

CRM A53G31.

Physical Description: 16-WT.
 

CRM A53C19.

Physical Description: 16-WT.
 

CRM A53L17. AB-65.

Physical Description: 16-ft.
 

CRM A53L03. AB-63.

Physical Description: 16-Foot.
 

RM A53K24. AB-59.

Physical Description: 16-Foot.
 

CRM A53121.

Physical Description: 16-Foot.
 

CRM A53J14.

Physical Description: 6x6.
Box Box 49

AG-62. RM A53J14a.

Physical Description: 6x6.
 

AG-66. CRM A53K20.

Physical Description: 6x6.
 

RM A53A30.

Physical Description: 6x6.
 

AG-67. CRM A53L22.

Physical Description: 6x6.
 

CRM A53L21. AG-69.

Physical Description: 6x6.
 

CRM A53D27.

Physical Description: 6x6.
 

CRM A53H18.

Physical Description: 6x6.
 

RM A53D10.

Physical Description: 1x3.
 

RM A53A13.

Physical Description: 1x3.
 

RM A53A09.

Physical Description: 1x3.
 

AE-81. A53D29.

Physical Description: 1x3.
 

AE-83. RM A53G08.

Physical Description: 1x3.
 

RM A53F12. AE-80.

Physical Description: 1x3.
 

CRM A53E28.

Physical Description: 1x3.
 

RM A5317.

Physical Description: 1x3.
 

A53F22.

Physical Description: 1x3.
Box Box 50

Seth B. Anderson. Flt. Research. AH-73. CRM A53G22. Original Text [hereafter refered to as O.T.]

 

Carlton S. James and Robert J. Carros. A0-7. SSFF. CRM A53D02. O.T.

 

Loris H. Ball. AG-66. CRM A53K20. O.T.

Physical Description: 6x6.
 

Sherman Edwards and Katsumi Hideko. AG-58. CRM A53H18 O.T.

Physical Description: 6x6.
 

Carl D. Kolbe and Frederick W. Boltz. AF-52. CRM A53L29. O.T.

Physical Description: 12 foot.
 

Frank A. Lazzeroni. AG-69. CRM A53L21. O.T.

Physical Description: 6x6.
Box Box 51

Carl D. Kolbe and Frederick W. Boltz. AF-52. CRM A53L29 O.T.

Physical Description: 12 foot.
 

Walter E. McNeill, Fred J. Drinkwater III and Rudolph D. Van Dyck, Jr. Flt. Res. AH-74. RM A53H10. O.T.

 

Earl C. Watson. AA-59. RM A53H03. O.T.

Physical Description: 7x10.
 

George Holdaway. Flt Eng. AK-25. CRM A53B16. O.T.

 

David E. Reese, Jr. AG-60. CRM A53D27. O.T.

Physical Description: 6x6.
Box Box 52

Bandettine and Selan. RM A53J07. AF-49. O.T.

Physical Description: 12-foot.
 

Fred A Demele. and William R. Otey. AF-43. RM A53F16. O.T.

Physical Description: 12-foot.
 

William C. Drake. AE-79. RM A53F22. O.T.

Physical Description: 1x3.
 

Leland Jorgensen. AE-80. CRM A53F12. O.T.

Physical Description: 1x3.
 

Matthews and Schmidt. AH-67. CRM A53B11. O.T.

 

A.J. Molk and R. M. Reunolds. AF-54. 12-foot CRM A53L29a. O.T.

 

Rathert, Gadeberg and Fiff. AH-70. Flt Res. RM A53H12. O.T.

 

Robert M. Reynolds. AF-56. RM A53J02. O.T.

Physical Description: 12-foot.
 

Ralph Selan and Angelo. Bondettini. AF-48. CRM A53 E12. O.T.

Physical Description: 12-foot.
Box Box 53

Scherrer, Stroud and Swift. CRM A53A13. AE-78. O.T.

Physical Description: 1x3.
 

Ralph Selon and Angelo Bondettini. AF-48. CRM A53E12. O.T.

Physical Description: 12-Ft.
 

Donald W. Smith and Verlin D. Reed. CRM A53C20. 12-foot. AF-45. O.T.

Physical Description: [2 Envelopes]
Box Box 54

J. Richard Spahr and Robert R. Dickey. AE-64. CRM A53D10. O.T.

Physical Description: 1x3.
Box Box 55

Edwin C. Allen. 16-foot. CRM A53C19. AB-55. O.T.

Physical Description: [2 envelopes]
 

M. Abromovitz, S.Schmidt, R. Van Dyck, Jr. AH-69. RM A53E21. O.T.

 

John A. Axelson. AB-60. 16 Wind Tunnel. CRM A53I23. O.T.

 

Richard S. Bray. Flt Res. AH-71. RM A53F23. O.T.

 

Joseph W. Cleary and Lee E. Boddy. AB-56. CRM AF3I21.

Physical Description: 16-Foot.
 

Charles F. Coe and Jack A. Mellenthin. AB-59. RM A53K24. O.T.

Physical Description: 16-foot.
Box Box 56

Horace F. Emerson. AB-63. RM A53L03. O.T.

Physical Description: 16-Foot.
 

McFadden, McCloud and James. Flt Res. AH-66. CRM A53A15. O.T.

Physical Description: 40x80.
 

Jack A. Mellenthin. AB-40. TN 3036. O.T.

Physical Description: 16-Foot.
 

Warren H. Nelson. AB-65. RM A5317. O.T.

Physical Description: 16.
 

Verlin Reed and Donald W. Smith. AF-46.

Physical Description: 12-foot O.T.
Box Box 57

L. Stewart Rolls. Flt. Res. AH-54. CRM A53A06. O.T.

 

Melvin Sadoff. Flt. Res. I.D. AH-64. RM A53G10. O.T.

 

Bruce E. Tinling and Armando Lopez. AF-47.

Physical Description: 12-foot O.T.
Box Box 58

N.K. Delany and N.E. Sorensen. AA62. TN 3038. O.T.

Physical Description: 7x10.
 

David Graham. AD-54. CRM A53D14. O.T.

Physical Description: 40x80.
 

Albert D. Hemenhover. RM A53G09. O.T.

Physical Description: 1x3½.
 

Albert D. Hemenhover. I.D. No AC 30. TN 2998. O.T.

Physical Description: 1x3½.
 

Hopkins and Carel. AA61. O.T.

Physical Description: 7x10.
 

Lynn W. Hunton and Harry A. James. AD-67. TN 3040. O.T.

Physical Description: 40x80.
 

Earl D. Knechtel. AC-34. TN 3087. O.T.

Physical Description: 1x3½.
 

David G. Koenig. Ad-66. RM A53D21. O.T.

Physical Description: 40x80.
 

Robert B. Petersen. AG-65. CRM A53J14. O.T.

Physical Description: 6x6.
Box Box 59

Vernon L. Rogallo and John L. McCloud III. AD-65. TN 2957. O.T.

Physical Description: 40x80.
 

Rough Draft. RM SA53C17. AG-61. Willard G. Smith O.T.

 

Stivers, Louis Jr. RM A53K06. AC-31. O.T.

Physical Description: 1x3-½.
Physical Description: 2 envelopes.
 

Benton E. Wetzel and Frank A. Pfyl. AG-62. RM A53J14a.

Physical Description: 6x6.
Box Box 60

Norman R. Bergrun and Paul A. Nickel. Flt Engr. AK-31. TN 2985.

 

G.B. Brajnikoff and J.F. Stroud. AE-87. CRM A53E28. O.T.

Physical Description: 1x3.
 

Benjamin R. Briggs and Arthur L. Jones. AL-53. Theo Aero. TN 2977. O.T.

 

Doris Cohen and Morris D. Friedman. Theo Aero. AL-52. TN 2959. O.T.

 

R.E. Dannenberg and J.A. Weiberg. AA-64. TN 3093. O.T.

Physical Description: 7x10.
 

Alson C. Frazer and Warren E. Anderson. AE-81. RM A53D29. O.T.

Physical Description: 1x3.
 

Forrest E. Gowen. AE-74. Conf RM A53A09. O.T.

Physical Description: 1x3.
 

Forrest E. Gowen. AE-84. RM A53117. O.T.

Physical Description: 1x3.
Box Box 61

George Holdaway. AK-33. Flt Engr. RM A53H17. O.T.

 

John A. Kelly and Nora Lee F. Hayter. AA-63 TN 3007. O.T.

Physical Description: 7x10.
 

Harvard Lomax. Theo. Aero. AL-50. TN 2925. O.T.

 

Carr B. Neel, Jr. AK-32. Flt Engr. TN 3025. O.T.

 

Stanford E. Neice. AN-15. TN 2694. O.T.

Physical Description: 10x14.
 

Spiegel, Hoffstetter and Kuehn. High Speed Res. and Unitary. AE-89. RM A53I01. O.T.

 

Syvertson and Gloria. AN-16. A53B02. O.T.

Physical Description: 10x14.
 

TN 2982. Milton D. Van Dyck. Theo. Aero. AL-54. O.T.

Box Box 62

CRM A54J07. AL-55. Theo Aero. 1954

 

TN 3390. AL-60. Theo. Aero. 1954

 

AL-60. TN 3283. Theo. Aero. 1954

 

TN 3286. AL-58. Theo Aero. 1954

 

TN 3343. AL-63. Theo Aero. 1954

 

TN 3345. AL-64. Theo Aero. 1954

 

TN 3389. AL-67. Theo Aero. 1954

 

* RM A54J19. AC-36. 1954

Physical Description: 2x2.
 

* RM A54H23. AE-99. 1954

Physical Description: 1x3.
 

TN 3227. AE-82. 1954

Physical Description: 1x3.
 

AE-90. TN 3128. 1954

Physical Description: 1x3.
 

TN 3344. AE-98. 1954

Physical Description: 1x3.
 

AO-12. SSFF. RM A53L18 1954

Box Box 63

TN 2900. Theo. Aero. AL-48. 1953

 

Theo Aero. TN 2727. 1953

 

TN 2925. Theo Aero. AL-50 1953

 

TN 2744. Theo Aero. 1953

 

Theo Aero. TN 2982. AL-54. 1953

 

TN 3173. AL-49. Theo Aero. 1953

 

TN 2977. AL-53. 1953

 

RM A53D02. SSFF. 1953

 

TN2919. H. Julien Allarn 1953

 

RM A53802. AN-16. 1953

Physical Description: 10x14.
 

RM A53D28. 1953

Physical Description: 10x14.
 

AF-49. CRM A53J07.1953

Physical Description: 12-Ft.
 

RM A53J02. 1953

Physical Description: 12-Foot.
Box Box 64

CRM A53L29a. 1953

Physical Description: 12
 

CRM A53I28. 1953

Physical Description: 12
 

AF-47. CRM A53D06. 1953

Physical Description: 12-Foot.
 

CRM A53F16. 12-Fppt. 1953

 

CRM A53A30a. AF-44. 1953

Physical Description: 12.
 

AF-55. RM A53L15. 1953

Physical Description: 12-Foot.
 

AF-51. CRM A53J23. 1953

Physical Description: 12-Foot.
 

RM A53L29. AF-52. 1953

Physical Description: TAR 12-Foot.
 

CRM A53C20 and RM A53H17 1953

 

CRM A53C20. AF-45. 12. 1953

Box Box 65

CRM A53F03. 12. 1953

 

RM A53E12. 1953

Physical Description: 12-Ft.
 

NACA RM A53B06. 1953

Box Box 66

Alfred G. Boissevain. SSFF. AO-11. RM A54B15a. O.T.

 

Thomas B. Carniny. AO-10. RM A54H23a. SSFF. O.T.

 

John C. Heitmeyer. RM A54B16. AG-71. O.T.

Physical Description: 6x6.
 

Willard G. Smith. CRM A54D05. AG-70. O.T.

Physical Description: 6x6.
 

Benton E. Wetzel. Ag 73. RM A54H26b. O.T.

Physical Description: 6x6.
 

Stanford E. Neice. AN 25. CRM A54C04. O.T.

Physical Description: 10x14.
 

David H Dennis and Bernard E. Cunningham. CRM A54E03. AN_24. O.T.

Physical Description: 10x14.
 

A.J. Eggers, Jr., and Clarence A. Syvertson. AN-26. RM A54J13. O.T.

Physical Description: 10x14.
 

A.J. Eggers, Jr., and C.A. Hermach. RM A54L13. AN-28. O.T.

Physical Description: 10x14.
 

Herrera and Barnes. AB-62. CRM A54A29. O.T.

Physical Description: 16-Foot.
 

John A. Wyss and James C. Monfort. AB.57. O.T.

Physical Description: 16-ft.
Box Box 67

Mossman and Anderson. RM A54B08. AE-93. Test.

Physical Description: 1x3.
 

George E. Kaaltari. RM A54D19. AE-101. O.T.

Physical Description: 1x3.
 

Spahr, L. Richard. AE-52. RM 54H27. O.T.

Physical Description: 1x3.
 

Kaaltari, George E. AE-105. CRM A54J12. O.T.

Physical Description: 1x3.
 

Gadeberg and Rathbert. Flight Research. AH-85. RM A54K16. O.T.

 

Abromovitz, Marivn; Van Dyke, Jr., Rudolph D. AH-86. CRM A54128. Flt Res. O.T.

 

Howard L. Turner, William C. Triplett, John S. White. Flt Res. AH-83 RM A54J14. O.T.

Box Box 68

AH-79. Flt Res. RM A54A05. O.T. L.Stewart Rolls and C. Dewey Havill.

 

Graham, David. AD-82. RM SA54I29.

Physical Description: 40x80.
 

Canning and Denardo. RM SA54C10. A0-8. SSFF.

Box Box 69

Ralph W. Franks. RM A54H26. AD-76. O.T.

Physical Description: 40x80.
 

Ralph W. Franks. RM A54H26a. AD-77. O.T.

Physical Description: 40x80.
 

Ralph L. Maki and Ursel R. Embry. CRM A54E10. AD-68. O.T.

Physical Description: 40x80.
 

David G. Koenig. AD-70. CRM A54B09. O.T.

Physical Description: 40x80.
 

Mark W. Kelly and William H Tolhurst, Jr. AD-71. CRM A54A25. O.T.

Physical Description: 40x80.
 

AA-65. TN 3094. O.T. Dannenberg. Weiberg and Gambucci.

Physical Description: 7x10.
 

James R. Blackaby and Earl C. Watson. AA-66. TN3170. Test

Physical Description: 7x10.
 

John A. Kelly and George B. Mc Cullough. AA-68. TN3220. Positive

Physical Description: 7x10.
 

Weiberg, James A. and Robert E. Dannenberg. AA-67. TN 3285. O.T.

Physical Description: 7x10.
Box Box 70

Robert E. Dannenber, James A. Weiberg and Bruno J. Gambucci. AA-73. TN 3388. O.T.

Physical Description: 7x10-foot.
 

Fred A. Demele and William R. Otey. AF-61.

Physical Description: 12-foot CRM A54
 

Jack D. Stephenson, Angelo Bandettini, and Ralph Selan. AF-62. RM A54K09. O.T.

Physical Description: 12-foot
 

Sutton and Dickson. AF-63. CRM A54F18. O.T.

Physical Description: 12-foot.
Box Box 71

Sammonds, Robert I and Reynolds, Robert H. AF-60. RM A54G14. O.T.

Physical Description: 12 ft.
 

George C. Kenyon and Robert M. Reynolds. AF-57. 12 CRM A54B18a. O.T.

Box Box 72

Norman M. Mc Fadden and Donovan R. Heink. AH-82. ANCA RM A54F21. O.T.

 

Melvin Sadoff, Frederick H. Mattheson and Rudolph D. Van Dyke, Jr. AH-80. CRM A54C31. Flt Res. O.T.

 

Matheson and Van Dyke Jr.,. AH-77. NACA RM A54B26. Flt Res. O.T.

 

AB-54. TN 3129. O.T.

Physical Description: 16 Foot.
 

Joseph W. Cleary. RM A54B18. AB-64. O.T.

Physical Description: 16-Foot.
 

Jack A. Mellenthin. AB-67. RM A54L22. O.T.

Physical Description: 16-foot.
 

Wyss, John A. and Herrera, Raymond. AB-68. RM A54H12 O.T.

Physical Description: 16-Ft. WT.
 

Nelson, Warren H. and Frank, Joseph L. AB-66. RM A54H12a. O.T.

Physical Description: 16 Ft W/T.
 

Monfort, James C. and Wyss, John A. AB-69. RM A54122. O.T.

Physical Description: 16 ft.
Box Box 73

Marvin Shinbrot. TN 3288. AH-76. Flt Res. O.T.

 

Stanley F. Schmidt and William Triplett. Flt. Res. AH-78. TN 3387. O.T.

 

Bradford H. Wick. AD-74. TN 3221. O.T.

Physical Description: 40x80.
 

John DeYoung and W.H. Barbing. AD-51. TN 3346. O.T.

Physical Description: 40x80.
 

Rogallo, McCloud III, and Yaggy. AD-79. CRM A54C30. O.T.

Physical Description: 40x80.
 

Cook, Woodrow L., Griffen, Roy N, Jr. and Hickey David H. AD-72. RM A54I21. O.T.

Physical Description: 40x80.
 

Constantine C. Pappas. AP-4. LDHT. TN 3222. O.T.

Box Box 74

Stalder and Nielsen. AP-6. TN 3287. Heat Transfer. O.T.

 

Morris W. Rubesin. AP-5. TN 3341. HT. O.T.

 

Lessing, Fryer and Mead. AG-75. TN 3348. O.T.

Physical Description: 6x6.
 

Eugene Migotsky. AG-72. TN 3386. O.T.

Physical Description: 6x6.
Box Box 75

Duane W. Dugan and Katsumi Hikido. AG-64. TN 3224. O.T.

Physical Description: 6x6.
 

Wetzel, Benton E. AG-76. CRM A54J20. O.T.

Physical Description: 6x6.
 

John C Heitmeyer. AG-68. O.T.

Physical Description: 6x6.
 

Louis S. Stivers, Jr. AC-35. TN 3127. Positives. Text.

Physical Description: 1x3½.
 

Robert E. Berggren and Donald J. Graham. AC-15. TN 3172. (formerly RM A50D04). O.T.

Physical Description: 2x2.
 

Barrett S. Baldwin. Jr., John B. Turner and Earl D. Knechtel. AC-28. O.T.

Physical Description: 1x3½.
 

Hemenover & Graham. AC-23. TN 3174. O.T.

Physical Description: 1x3½.
Physical Description: 2 Envelopes.
Box Box 76

Summers, James L., Treon, Stuart L., and Grahm, Lawrence A. AC-37. RM A54L20. O.T.

Physical Description: 2x2.
 

Barrett S. Baldwin and Robert R. Dickey. AC-36. RM A54J19. O.T.

Physical Description: 2x2.
 

Milton D. Van Dyke. TN 3173. Theo Aero. AL-49. O.T.

 

Alvin H. Sacks. TN 3283. AL 60. Theo Aero. O. Figures

 

J.M. Spiegel and Philips J. Tunnel. AW-1. Unitary. TN 3223. O.T.

 

Philips J. Tunnel. AW-2. RM A54K16a. Unitary. O.T.

Box Box 77

Simon C. Sommer and Barbara J. Short. SSFF. AO-17. TN 3391. O.T.

Box Box 78

A.C. Charters. SSFF. AO-16. TN 3350. O.T.

Box Box 79

James R. Jedlicka, Max E. Wilkins, and Alvin Seiff. SSFF. TN 3342. AO-12. O.T.

Physical Description: [Two Envelopes]
 

Seiff, Alvin. SSFF. AO-13. TN 3284. O.T.

 

Robert J. Carros and Carlton S. James. AO-13. SSFF. Tn 3171. O.T.N.D.

 

Thomas N. Canning. AO-14. SSFF. TN 3125. O.T.N.D.

 

Carr B Carr BltNeel. Flt Eng. AK-36. RM A54I23. O.T.N.D.

 

Carr B. Neel. Flt Eng. AK-35. TN 3130. O.T.N.D.

 

George H. Holdaway. RM A54I17. AK-38. Flt Eng. O.T.N.D.

Box Box 80

George H. Holdaway. Flt Eng. RM A54F22. R-9-T. O.T.N.D.

 

Bright, Loren G. Flt. Eng. AK-39. RM A54L27. O.T.N.D.

 

Maurice D. White. Flt Eng. AK-34. RM A54E12. O.T.N.D.

 

H.G. Stine and Kent Wanlass. AE-98. TN 3344. O.T.N.D.

Physical Description: 1x3.
 

William R. Wimbrow. RM A54A07. AE-96. O.T.N.D.

Physical Description: 1x3.
 

Arthur Wm Rogers. AE-82. TN 3227. O.T.N.D.

Physical Description: 1x3.
 

Vincenti, Dugan and Phelps. TN 3225. AE-92. O.T.N.D.

Physical Description: 1x3.
Box Box 81

D. Chapman and R. Kester. AE-91. TN 3097. O.T.N.D.

Physical Description: 1x3.
 

Warren E. Anderson and Richard Scheerer. AE-102. RM A54E06. O.T.N.D.

Physical Description: 1x3.
 

Meyer M. Resnikoff. RM A54B15. AN-23. O.T.N.D.

Physical Description: 10x14.
 

Eggers and Nothwang. AN-22. TN 3095. O.T.N.D.

Physical Description: 10x14.
 

CRM A54E06; CRM A54B15a.

Box Box 82

RM A54F21. AH-82. Flt Res. 1954

 

CRM A54B26. Flt Res. AH-77. 1954

 

CRM A54C31. AH-80. Flt Res. 1954

 

CRM A54H09. AH-84. Flt Res. 1954

 

RM A54J14. AH-83. Flt Res. 1954

 

RM A54K16. AH-85. Flt Res. 1954

 

CRM A54I28. AH-86. Flt Res. 1954

 

CRM A54E12. AK-34. Flt Res. 1954

 

RM A54F22. AK-37. Flt Eng. 1954

 

RM A54L27. AK-39. Flt Eng. 1954

 

RM A54I23. AK-36. Flt Eng. 1954

 

RM A54I17. AK-38. Flt Eng. 1954

 

RM A54B18. AB-64. Flt Eng. 1954

 

CRM A54A22. AB-50. 16-Foot. 1954

Physical Description: 16-Foot.
 

AB-62. CRM A54A29. 1953

Physical Description: 16-Foot.
Box Box 83

CRM A54C24. AB-57. 1953

Physical Description: 16-Foot.
 

CRM A54H12. AB-68. 1953

Physical Description: 16-Foot W/T.
 

RM A54H12a. AB-66. 16-Foot. 1953

Physical Description: 16-Foot.
 

RM A54L22. AB-67. 16-Foot. 1953

Physical Description: 16-Foot.
 

RM A54I22. AB-69. 16-Foot. 1953

Physical Description: 16-Foot.
 

AO-10. RM A54H23a. SSFF. 1953

 

CRM A54E03. AN-24. 1953

Physical Description: 10x14.
 

AN-23. RM A54B15. 1953

Physical Description: 10x14.
 

CRM A54C04. AN-25. 1953

Physical Description: 10x14.
 

RM A54J13. AN-26. 1953

Physical Description: 10x14.
 

CRM A54L10. AN-27. 1953

Physical Description: 10x14.
 

RM A54L13. AN-28. 1953

Physical Description: 10x14.
 

CRM A54K16a. AQ-2. Unitary 1953

 

RM A54L20. AC-37. 1953

Physical Description: 2x2.
Box Box 84

CRM A54D19. AE-101 1953

Physical Description: 1x3.
 

CRM A54B08. AE-93.

Physical Description: 1x3.
 

CRM A54B08a. AE-94.

Physical Description: 1x3.
 

RM A54A07. AE-96.

Physical Description: 1x3.
 

RM A54H27. AE-52.

Physical Description: 1x3
 

CRM A54J12. AE-101.

Physical Description: 1x3
 

CRM A54C30. AD-79.

Physical Description: 40x80.
 

RM A54E10. AD-68.

Physical Description: 40x80.
 

CRM A54A25. AD-71.

Physical Description: 40x80.
 

RM A54B09. AD-70

Physical Description: 40x80.
 

RM SA54109. AK-38.

Physical Description: 40x80.
 

RM 54N26. AD-76.

Physical Description: 40x80.
 

RM A54N26a. AD-77.

Physical Description: 40x80.
 

RM A54I21. AD-72.

Physical Description: 40x80.
 

RM A54I29. AD-82.

Physical Description: 40x80.
 

RM SA54B16. AG-71.

Physical Description: 6x6.
 

RM A54D05. AG-70.

Physical Description: 6x6.
Box Box 85

CRM A54A04. AG-68.

Physical Description: 6x6.
 

CRM A54J20. AG-76.

Physical Description: 6x6.
 

RM SA54H26b. AG-73.

Physical Description: 6x6.
 

CRM A54D22. AF-61.

Physical Description: 12-Foot.
 

CRM A54F14. AF-50.

Physical Description: 12-Foot.
 

CRM A54B18a. AF-57. 12.

 

RM A54F18. AF-63. 12.

 

AF-58. RM A54G13. 12.

 

RM A54G14. AF-60.

Physical Description: 12-Ft.
 

RM A54J22. AF-59. 12.

Box Box 86

RM A54K09. AF-62.

Physical Description: 12-Foot.
 

RM A54L07. AF-71.

Physical Description: 12-Foot
 

RM A54L08. AF-64.

Physical Description: 12 Foot.
 

RM A54F28. Theo Aero.

 

TN 3171. AO-13. SSFF.

 

TN 3388. AA-73.

Physical Description: 7x10.
 

RM A54A05. AH-79. Flt Res.

 

TN 3387. AH-78. Flt Res.

 

TN 3288. AH-76. Flt. Res.

 

TN 3346. AD-51.

Physical Description: 40x80.
 

TN 3287. AP-6. Heat Transfer.

Box Box 87

RM A54L27 by Bright.

 

RM A54F22. by Holsaway. 1954.

 

TN 3130. "The Design of Air-Heated Ice Prevention Systems" by Carr B. Neel. 1953-1954.

 

RM A54I17. by Holdaway. 1954.

 

RM A54I23. By Carr Neel.

 

RM A54E12. By Maurice D. White.

 

CRM A55F21. By Maurice D White. 1955.

 

CRM A55F06. By George H. Holiday. 1955.

 

CRM A55D18. By Maurice D. White. 1955.

Box Box 88

TN 3670. AL-74. Theo. Aero. Alberta Y. Alksne.

 

RM A56F15. AN-48. HSR. H. Julian Allen. N.D.

 

RM A56G30. AH-109. Flt Res. Seth B. Anderson, Hervey C. Quigley and Robert C. Innis. N.D.

 

RM A56110. AH-113. Flt. Res. Robert M. Barnett, William M. Kaufman and Elmer C. Fulcher. N.D.

 

RM A56G17. AF-87. Frederick W. Boltz, George C. Kenyon, Clyde Q. Allen. N.D.

Physical Description: 12-foot.
 

TN 3874. AH-112. Flt Res. Brown, Stuart C., and Holleman, Euclid C. N.D.

 

RM A56104. AF-77. Donald A. Buell, Verlin D. Reed, and Armando E. Lopez N.D.

Physical Description: 12-foot.
 

RM A56H06. AF-85. Donald A. Buell, and Bruce R. Tinling. N.D.

Physical Description: 12-foot.
 

TN 3718. AL-72. Theo. Aero. Paul F. Byrd. N.D.

 

RM A56B15. AO-21. SSFF. By Robert J. Carros. N.D.

 

TN 3792. AE-127. Dean R. Chapman. N.D.

Physical Description: 1x3.
Box Box 89

RM A56H30. AH-111. Flt. Res. Creer, Brent Y. N.D.

 

TN 3669. AA-82. Dannenberg, Gambucci, and Weinberg. N.D.

Physical Description: 7x10.
 

RM A56C06. AE-116. Wallace F. Davis and Forrest E. Gowen. N.D.

Physical Description: 1x3.
 

RM A56E23. AC-46. Robert E. Dickey N.D.

Physical Description: 2x2.
 

RM A56C01. AA-81. Jules B. Dods, Jr., and Earl C. Watson. N.D.

Physical Description: 7x10.
 

RM A56D06. AF-80. George G. Edwards and Howard F. Savage. N.D.

Physical Description: 12 foot.
 

TN 3789. AF-82. Feorge G. Edwards, Jerald K. Dickson, Fred B. Sutton and Fred A. Demele. 1954.

Physical Description: 12 foot.
 

TN 3790. AF-83. Feorge G. Edwards, Donald A. Buell, Fred A. Demele, and Fred B. Sutton. (Supercedes RMs A53J23 and A 54F14). 1954.

Physical Description: 12 foot.
 

RM A56B17. AD-89. William T. Evans N.D.

Physical Description: 40x80.
 

CRM A56G24. AH-106. Flt Res. Jos. G. Dowillier, Jr. J.V. Foster, and F.J. Drinkwater III. N.D.

 

TN 3797. AA-87. Bruno J. Gambucci. N.D.

Physical Description: 7x10.
Box Box 90

TN 3964. AB-83. McDevitt, John B.

Physical Description: 14 foot.
 

TN 4231. AF-90. Donald E. Gault

Physical Description: 12 foot.
 

TN 3963. AF-88. Smith Donald W, and Walker, John H.

Physical Description: 12 foot.
 

NACA TN 144. AO-27. SSFF. Steve P. Heins.

 

TN 4230. AO-29. SSFF. Steve P. Heins.

 

TN 3962. AN 47. C. Frederick Hansen.

Physical Description: 10x14.
 

TR 1328. (Supercedes NACA TN 3527). AN-56. Clarence A. Syvertson and David H. Dennis.

Physical Description: 10x14.
 

TN 4229. AN-62. Eggers, A.J., Jr., Hansen, C. Frederick, and Cunningham, Bernard E.

Physical Description: 10x14.
 

TN 4046. AN-29. Alfred J. Eggers, Jr., H. Julian Allen, Stanford E. Neice.

Physical Description: 10x14.
 

TN 3290. AG-103. Murray Tobak.

Physical Description: 6x6.
 

TN 3290. AE-120. Darren Winovich and Howard A. Stine.

Physical Description: 1x3.
 

TN 4146. AE-133. Spahr, J. Richard.

Physical Description: 1x3.
 

TN 3869. AE-119. Dean R. Chapman, Donald M. Kuehn, and Howard K. Larson.

Physical Description: 1x3.
Box Box 91

RM A56H27. AN-49. Hermilo R. Gloria. N.D.

Physical Description: 10x14.
 

RM A56B27. AD-81. Griffen and Hickey N.D.

Physical Description: 40x80.
 

TN 3714. AH 108. Flt Res. C. Dewey Havill and L. Stewart Rolls. N.D.

 

TN 3868. AL-78. Theo Areo. Max. A. Heaslet and Franklin B. Fuller. N.D.

 

Max. A. Heaslet and John R. Spreiter. TN 3717. AL 73. Theo Aero N.D.

 

RM A56L05. AN-52. C.A. Hermach, Samual Kraus, and John O. Reller, Jr. N.D.

Physical Description: 10x14.
 

RM A56118. AE-128. Daniel P. Hickey. N.D.

Physical Description: 1x3.
 

RM A56C12. AE-118. William A. Hill, Jr., and George E. Kaatari. N.D.

Physical Description: 1x3.
 

RM A56K26. AB-82. 14. Holdaway, George H., and Hatfield, Elaine W. N.D.

 

RM A56F01. AD-88. Curt A. Holzhauser, Robert K. Martin, and V. Robert Page. N.D.

Physical Description: 40x80.
 

TN 3793. AD-98. Holtzhauser, Curt A., and Hall, Leo. P. N.D.

Physical Description: 40x80.
 

TN 1270. AD-90. By Curt A. Holzhauser and Richard S. Bray. (Supercedes RM's A52G17 and A55C07). N.D.

Physical Description: 40x80.
 

RM A56G16. AE-126. Leland H Jorgensen and Elliot D. Katzen. N.D.

Physical Description: 1x3.
Box Box 92

RM A56712. AD-91. Kelley, Mark W.

Physical Description: 40x80.
 

RM A56G19. AD-96. Mark W. Kelly and Jeffry H. Tucker.

Physical Description: 40x80.
 

RM A56H31. AC-45. Earl D. Kuechtel and Arvid N. Andrea.

Physical Description: 2x2.
 

RM A56D23. AD-93. David M. Koeing.

Physical Description: 40x80.
 

RM A56H08. AD-94. Koenig, David G., and Aoyagi, Kiyoshi.

Physical Description: 40x80.
 

Technical Report (Supercedes RM A55B16). AL-80. Theo. Aero. Howard Lomax and Max. A. Heaslet.

 

TN 3871. AD-84. Maki, Ralph L, and Hunton, Lynn W.

Physical Description: 40x80.
 

RM A56F07. AH-107. Flt. Res. Howard F. Matthews and Robert B. Merrick.

 

TR 1295. AD-97. Vernon L. Rogallo, Paul F. Yaggy, and John L. McCloud III.

Physical Description: 40x80.
 

RM A56C08. AH-103. Flt. Res. McNeill, Walter E., and Creer, Brent Y.

 

RM A56G06. AG-99. Emmet A. Mossman and Frank A. Pfyl.

Physical Description: 6x6 ft.
 

TN 3722. AE-106. Jack N. Nielsen and William C. Pitts. (Formerly RM A55B07).

Physical Description: 1x3.
Box Box 93

TN 3873. AE-130. Jack N. Nielson.

Physical Description: 1x3.
 

TN 3721. AN-46. George J. Nothwag.

Physical Description: 10x14.
 

TN 3872. AC-48. William A. Page

Physical Description: 2x2.
 

RM A56107. AG-94. Robert B. Peterson.

Physical Description: 6x6.
 

RM A56L18. AG-102. Peterson, Victor L., and Boyd, John W.

Physical Description: 6x6.
 

RM G56AB03. AG-89. E. Ray Phelps.

Physical Description: 6x6.
 

TR 1307. AE-135. William C. Pitts, Jack N. Nielson, and George E. Kaatlari.

Physical Description: 1x3.
 

Alvin H. Sacks. TN 3725. AL-75. Theo Areo.

 

AL-83. Sacks. Theo Aero. TN 3796.

 

RM A56D02. AF075. Robert S. Sammond and Robert F. Reynolds.

Physical Description: 12-foot.
 

TN 3668. AE-114. Scherrer, Richard and Anderson, Warren E.

Physical Description: 1x3.
 

RM A56K07. AH-110. Flt Res. Schmidt, Stanley F., Bergun, Norman F., Merrick, Robert B., and Matthews, Howard F.

Box Box 94

RM A56I05. A0-24. SSFF. Alvin Seiff, Simon C. Sommer, and Thomas N. Canning.

 

TN 3791. AH-105. Flight Research. Marvin Shinbrot.

 

TN 3720. AA-74. Norman E. Sorensen and Edward J. Hopkins.

Physical Description: 7x10.
 

John R. Spreiter, and Alvin H. Sacks. TN 3528. AL-44. Theo. Aero.

 

RM A56B27a. AP-9. LDNT. Jackson R. Stalder and Mamoru Iouye.

 

RM A56B21. AE-112. Howard A. Stine and Warren Winovich.

Physical Description: 1x3.
 

RM A56E22. AC-42. Summers, Treon and Graham.

Physical Description: 2x2.
 

RM A56J08. AF-81. Fred B. Sutton and J. Walter Lautenberger.

Physical Description: 12-foot.
 

RM A56111. AN-50. Clarence A. Syvertson. Thomas J. Wong, and Hermilo R. Gloria.

Physical Description: 10x14.
 

RM A56D05. AP-12. Heat Transfer. By Thorval Tendeland and Arthur F. Okuno.

 

TN 3788. AG-98. Murray Tobak and William R. Wekrend.

Physical Description: 6x6.
 

RM A56E24. AD-92. William H. Tolhurst, Jr., and Mark W. Kelly.

Physical Description: 40x80.
Box Box 95

RM A56K19. AH-114. Flt Res. William C. Triplett, John D. McLean, John S. White.

 

TR 1274. AL-77. Theo. Aero. By Milton D. Van Dyke. (Supercedes TN's 3390 and 3343).

 

TN 3875. AL-79. Theo Aero. Milton D. Van Dyke.

 

TN 3723. AE-113. Walter G. Vinventi, Cleo B. Wagoner, and Norman H. Fisher, Jr.

Physical Description: 1x3.
 

RM A56A06. AN-44. By Thomas J. Wong and Hermilo R. Gloria.

Physical Description: 10x14.
Box Box 96

NACA TN 4045. AE-141. Leland H. Jorgensen

Physical Description: 1x3.
 

TN 3967. ID.No. AE-134. Frank J. Centolanzi.

Physical Description: 1x3.
 

TN 4149. AP-18. LDHT. Morris W. Rubesin and Constantine C. Pappas.

 

TN 4142. AP-16. LDHT. Marcus O. Creager.

 

TN 3969. AP-13. LDHT. Morris W. Rubesin and Mamoru Inouye.

 

TN 4141. AP-15. LDHT. Jackson R. Stalder.

 

TR 1330. AN-134. Flt Res. (Supercedes NACA RM A54H09 and TN 3874) Henry A. Cole Jr., Stuart C. Brown, and Euclid C. Holleman.

 

RM A57G10. AHO120. Flt. Res. Seth B. Anderson, Alan E. Faye, Jr., and Robert C. Innis.

 

TN 4147. AH-128. Flt Res. Cole, Henty A., Jr., and Holleman, Euclid C.

 

TN 4145. AH-135. Flt Res. Shinbrot, Marvin and Carpenter, Grace C. N.D.

 

TN 3968. AH-123. Flt Res. Brian F. Doolin N.D.

 

TN 4148. AL-94. Theo. Aero. By John R. Spreiter, Alberta Y. Alksne, and B. Jeanne Hyett. N.D.

 

RM A57H21. AD-101. David G. Koenig and Kiyoshi Aoyagi. N.D.

Physical Description: 40x80.
Box Box 97

RM A57K01. AD-106. Curt A. Holzhauser.

Physical Description: 40x80.
 

TN 4227. AL-95. Theo. Aero. Max A. Heaselet and Franklin B. Fuller.

 

TN 3289. AL-93. Theo Aero. Max A. Heaselet

 

TN 4232. AL-91. Theo Aero. Harvard Lomax and Loma Sluder.

 

TN 4038. AA-86. Robert E. Dannenberg, James A. Weiberg, and Bruno J. Gambucci.

Physical Description: 7x10.
Box Box 98

RM A57J16. AB-877. By John A. Axelson.

Physical Description: 14 Foot
 

RM 57N19a. AB-86. George H. Holdaway, Minor R. Wallace, Jr., and Elain W. Hatfield

Physical Description: 14 foot.
 

RM A57G01. AB-84. By Joseph W. Cleary, Joseph L. Frank, and Forbes Dewey.

Physical Description: 14 foot.
 

RM A57E23. AB-85. By George H. Holdaway and Minor R. Wallace Jr.

Physical Description: 14 foot.
 

RM A57A02. AB-80. 14. McDevitt, John B., Taylor, Robert A.

 

RM A57F03. AD-104. David H. Hickey.

Physical Description: 40x80.
 

RM A57D11. AD-100. James, Harry A. and Maki, Ralph L.

Physical Description: 40x80.
 

RM A57B11. AD-99. William T. Evans.

Physical Description: 40x80.
 

RM A57A24. AD-95. Ralph L. Maki and Harry A. James.

Physical Description: 40x80.
 

RM A57F06a. AF-89. 12. Sutton, Fred B., and Lautenberger, J.Walter Jr.

 

RM A57E02. AF-84. Donald A. Buell and Carl D. Kolbe.

Physical Description: 12-foot.
 

RM A57H19. AF-99. Demele, Fred A.

Physical Description: 12-foot.
 

RM A57K05. AF-100. Bruce E. Tinling.

Physical Description: 12-foot.
 

RM A57130. AN-59. David H. Dennis.

Physical Description: 10x14.
Box Box 99

RM A57126. AN-55. By Neice, Carson, and Cunningham.

Physical Description: 10x14.
 

RM A57F03a. AN-54. John O. Reller, Jr.

Physical Description: 10x14.
 

RM A57K20. AT-9. A. Vernon Gros. and Richard L. Kurkowski.

Physical Description: 9x7.
 

RM SA57F06. AT-1. Hofstetter, William R.

Physical Description: 9x7.
 

RM A57126a. AT-2. Norman D. Wong.

Physical Description: 9x7.
 

RM A57C25. AO-26. SSFF. Thomas N. Canning. and Simon C. Sommers.

 

RM A57I09. AC-52. By George Leland James L. Summers.

Physical Description: 2x2.
 

RM A57F06b. AC-50. Earl D. Knechtel and George Lee.

Physical Description: 2x2.
 

RM A57I10. AC-43. Stivers, Louis S., Jr., and Lippman, Garth W.

Physical Description: 2x2.
 

RM A57A25. ID AC-51. Stuart L. Treon and Earl D. Knechtel.

Physical Description: 2x2.
 

RM A57L23. AE-146. Nielsen, Jack N.

Physical Description: 1x3.
 

RM A57I17. AE-131. By William A. Hill, Jr.

Physical Description: 1x3.
 

RM A57E21. AE-140. Spahr. J. Richard and Polhamus, Edward C.

Physical Description: 1x3.
 

RM A57K21. AP-17. LDHT. Neel, Carr B.

 

RM A57K21. AP-14. LDHT. Helmer V. Nielsen.

 

RM A57K21. AH-113. Flt Res. William C. Triplett

 

RM A57K21. AH-127. Flt Res. Maurice D. White, Bernard A. Schlaff, and Fred J. Drinkwater III.

 

RM A57L10. AH-129. Flt Res. McFadden, Pauli, and Heinle.

 

RM A57K07. AH-131. Flt Res. Sadoff and Stewart.

Box Box 100

RM A57J01. AH-121. Flt Res. Howard L. Turner, George A. Rathert, Jr. and Donovan R. Heinle

 

RM A57D30. AH-119. Flt Res. Maurice D. White and Fred J. Drinkwater

 

RM A57D09. AH-125. Flt Res. William C. Triplett and Francis W.K. Hom.

 

RM A57D04. AH-118. Flt Res. Melvin Sadoff, John D. Stewart and George E. Cooper.

 

RM A57C19. AH-117. Flt. Res. Foster, Fulcher, and Heinle.

 

RM A57B14. AH-115. Flt. Res. Hervey C. Quigley, Francis W.K. Hom, and Robert C. Innis.

 

RM A57L18. AG-111. Victor L. Peterson and Gene P. Meness.

Physical Description: 6x6.
 

RM A57K27. AG-114. Victor L. Peterson and John W. Boyd.

Physical Description: 6x6.
 

RM A57K26. AG-113. Victor L. Peterson and Meness, Gene P.

Physical Description: 6x6.
 

RM A57K14. AG-112. Victor L. Peterson and John W. Boyd.

Physical Description: 6x6.
 

RM A57J22. AG-105. David E. Reese, Jr.

Physical Description: 6x6.
 

RM A57J15. AG-108. Vicotr L. Peterson and John W. Boyd.

Physical Description: 6x6.
 

RM A57E22. AG-97. Willard G. Smith and Peter F. Intrieri.

Physical Description: 6x6.
 

RM A57A10. AG-101. E. Ray Phelps and John W. Boyd.

Physical Description: 6x6.
 

RM A57E15. AG-95. Migotsky, Eugene and Adams, Gaynor J.

Physical Description: 6x6.