Albert Yackle papers

Kellett Aircraft Corporation

Box 1

Airborne Support Platform - American Helicopter Society, Inc.

Folder 1

Kellett Aircraft Corporation -- Airborne Support Platform. Preliminary Design Report No. 173X90-2, (1960)

Airborne Support Platform, Preliminary Design Report No. 173X90-2; Report of Army Member to Subcommittee on Aircraft Loads; technical data; and printed matter

Folder 2

Kellett Aircraft Corporation -- Aircraft - Army Requirements Civilian Requirements, (1958)

Correspondence with Asplundh Tree Expert Company, Kellett Aircraft Corporation Two-Place Helicopter, and printed matter

Folder 3

Kellett Aircraft Corporation -- Aircraft Propeller Handbook, (1956)

Issued Jointly by Department of the Air Force and Department of the Navy

Folder 4

Kellett Aircraft Corporation -- Airfoil, (1939-1945)

National Advisory Committee For Aeronautics. Summary of Airfoil Data Report No. 824 and The Characteristics of 78 Related Airfoil Sections From Tests in the Variable-Density Wind Tunnel Report No. 460

Folder 5

Kellett Aircraft Corporation -- The Alouette II, (1956-1957)

Republic Aviation Corporation

Folder 6

Kellett Aircraft Corporation -- American Helicopter Society, Inc, (1956-1960)

Third and sixteenth conference

Folder 7

Kellett Aircraft Corporation -- American Helicopter Society, Inc. (1969)

25th Annual National Forum Proceedings

Folder 8

Kellett Aircraft Corporation -- American Helicopter Society, Inc. (1973)

29th Annual National Forum

Box 2

Analysis of Structural Demonstration... - ASW - Droned Weapons System

Folder 1

Kellett Aircraft Corporation -- Analysis of Structural Demonstration and Strain Survey Records of Model YH-21 Report No. 22-T-34, (1954)

Piasecki Helicopter Corporation

Folder 2

Kellett Aircraft Corporation -- ANC Bulletin 18. Design of Wood Aircraft Structures, War Department Army Air Forces, (1944)

Army-Navy-Civil Committeefgf;

Folder 3

Kellett Aircraft Corporation -- Armed Services Technical Information Agency, (1953)

Design Criteria Extruded Blades Applied to Jacobs 104 Report No. 104-B-04; Preliminary Analysis Extruded Rotor Blade for Jacobs 104 Rotorcraft No. 104-B-03; Extruded Rotor-Blade Outline of Ground Tests for Blade Balance Program Report No. 104-T-16; Extrusion Process Applied to Rotor Blade Fabrication Part 1 General Investigation of Extrusion Process Report No. 104-B-01

Folder 4

Kellett Aircraft Corporation -- Armed Services Technical Information Agency, (1954)

Extruded Blade for Jacobs 104 Flexure-Torsion Flutter Analysis Report No. 104-V-01(2); Theoretical Aerodynamic Loads of the Jacob 104 Main Rotor Blades Part (3) Best Unaccelerated Autorotative Flight Condition Report No. 104A-04; Helicopter Ground Resonance, In Theory Experiment Report V. 1748; Outline of Extruded Blade Development Program Report No. 104-4-01; and Extruded Blade for Jacobs 104 Fatigue Analysis Interim Report #1 Report No. 104-B-11(1)

Folder 5

Kellett Aircraft Corporation -- ASW - Droned Weapons System, (1959)

Drone Anti-Submarine Weapon System Report No. 153X90-1; ASW Anti-Submarine Warfare report; Design Requirement; Design Proposal; and photograph

Box 3

Autogiro - Convertiplane Conference

Folder 1

Kellett Aircraft Corporation -- Autogiro, (1940-1960)

Correspondence from Eastern Air Lines to Kellett Autogiro Corporation and technical data

Folder 2

Kellett Aircraft Corporation -- Autogiro - Jump Take Off, (1938-1940)

Advanced Autogiro Theory by R.H. Prewitt; Report of Results of Miscellaneous Tests of XG1B Autogiro; notes; and technical data

Folder 3

Kellett Aircraft Corporation -- Autogiro Specifications, (1936-1946)

Performance Charts of Kellett Autogiros Report No. ER 160.4; Detail Specifications for Model YG-1A Autogiro Engine - Jacobs L-4-MA Contract No. W535-AC-8606…Spec. YG-1A No. 8-120.1; X-3 Performance Report No. 120.20; An Outline of Kellett Rotorcraft Development; Some Facts of Interest About Rotating - Wing Aircraft and the Autogiro Company of America; notes; and technical data

Folder 4

Kellett Aircraft Corporation -- Basic Data (miscellaneous), (1950-1953)

Stress-Strain and Tangent Modulus Curves; Comparison of Properties of 3 Ultura-High H.T. Steels; Bending Stresses in Curved Round Thin Tubes; Reamed Bolt Hole; Notes on Helicopter Calculations; Determination of Compression Springs with Minimum Compressed Lengths; Test Memorandum Report; and memorandums

Folder 5

Kellett Aircraft Corporation -- Bearings Oscillating, (1960)

Some Contributions to Ball Bearing Theory by A.B. Jones; correspondence from Shook, Gerald D. to Leonard Goland; Laminated Bearing for Helicopter Hub; and correspondence from Lawrence, John C. to Albert R. Yacklefv

Folder 6

Kellett Aircraft Corporation -- Bell 47 G, [undated]

Introducing the new Bell Model 47 G Helicopter product of over a million flight hours

Folder 7

Kellett Aircraft Corporation -- Bell Helicopter Certification, (1955)

Department of Commerce Civil Aeronautics Administration

Folder 8

Kellett Aircraft Corporation -- Brantly Helicopter Test Results, (1959)

Brantly B-2 pamphlet; Navy Evaluation of Army Model YHO-3BR Helicopter, Report No. 1; and price list

Folder 9

Kellett Aircraft Corporation -- Configuration Sketches - artist’s, (1957)

Notes on an Ideal Two Place Light Helicopter, technical data, and printed matter

Folder 10

Kellett Aircraft Corporation -- Convertible Aircraft Congress, (1958)

Fourth Convertible Aircraft Congress Proceedings, Philadelphia

Folder 11

Kellett Aircraft Corporation -- Convertiplane Conference, (1954-1960)

Observations on Subsonic V/STOL Aircraft Designs for the United States Airforce; K-25 Twin Engine Configuration; The Convertiplane. Implications of a New Aircraft Type on the National Aviation Policy of the United States; General Performance Analysis of a New Type 4-Place Utility Airplane; printed matter; and technical data

Box 4

Convertiplane - Dynamic Response

Folder 1

Kellett Aircraft Corporation -- Convertiplane K-25 Presentation, (1956-1958)

Kellett K-25 Convertiplane Presented at the Forth Convertible Congress and printed matter

Folder 2

Kellett Aircraft Corporation -- Convertiplane Principles, (1956)

Paper Presented at the Annual General Meeting of the Canadian Aeronautical Institute and The Kellett K-25 Flying Test Bed Report No. 106X90-1

Folder 3

Kellett Aircraft Corporation -- A Convertiplane Rotor System Design Study Report No. 106X90-3, (1957)

Folder 4

Kellett Aircraft Corporation -- A Convertiplane Rotor System Design Study Report No. 106X90-3, (1957)

Duplicate

Folder 5

Kellett Aircraft Corporation -- Cost Analysis Method - Hiller, (1954-1958)

Helicopter costs; Bell Model 47 Helicopter; clippings; notes; and xs Technical Information Agency. Aircraft Cost Analysis

Folder 6

Kellett Aircraft Corporation -- Cumulative Fatigue Damage of Aircraft Structural Materials Part 2: 2024 and 7075 Aluminum Alloy Additional Data and Evaluation by Alfred M. Fruedenthal and Robert A. Heller, (1956)

Folder 7

Kellett Aircraft Corporation -- Drag, Aerodynamic, (1960)

Aerodynamic Drag notes and The Problem of Aerodynamic Heating, E.R. van Driest, North American Aviation, Inc.

Folder 8

Kellett Aircraft Corporation -- Dynamic Response (a), (1957-1958)

The Kaman Aircraft Corporation. Dynamic Response of a Helicopter to a Gust, Part 1 Report No. R-30

Box 5

Dynamic Response - Helicopter - Plastic Fuselage

Folder 1

Kellett Aircraft Corporation -- Dynamic Response (b), (1957-1958)

The Kaman Aircraft Corporation. Dynamic Response of a Helicopter to a Gust, Parts 2-4 Report No. R-30

Folder 2

Kellett Aircraft Corporation -- Epicyclic Rotor System, (1952)

Proposal for the theoretical investigation of the Performance - Stability & Control. Characteristics of an Epicyclic Rotor System, Report no. 63X-80-1 and 2nd Convertible Aircraft Congress: Proceedings

Folder 3

Kellett Aircraft Corporation -- Experimental Study of a Tandem Helicopter Employing Cocked Vertical Blade Hinges by Peter F. Leone, (1956)

Folder 4

Kellett Aircraft Corporation -- Fatigue Problems in Helicopters - Maintenance, (1957-1958)

Experience of New York Airways, Inc. on Maintenance of Helicopters: An Address Before the Conference on Helicopters Called by the Aviation Division of the Army Transportation Service; memorandums; Skyways: Flight Operations-Engineering-Management; Cumulative Damage in Fatigue by Milton A Miner; papers regarding fatigue, Society of Automotive Engineers; notes; and correspondence

Folder 5

Kellett Aircraft Corporation -- Flight Manual for Model SO. 1221 Djinn Helicopter, (1958)

Folder 6

Kellett Aircraft Corporation -- Flying Crane Helicopter, (1957)

Report

Folder 7

Kellett Aircraft Corporation -- Frankford Arsenal Drone and Proposal, (1958-1959)

Tank Refueling by Helicopter, correspondence, and technical data

Folder 8

Kellett Aircraft Corporation -- The Franklin Institute, (1956-1957)

Research Proposal for Kellett Aircraft Corporation on Design and Development of a Set of Hydrostatic Rotor Blade Root Retention Bearings, blueprints, and correspondence

Folder 9

Kellett Aircraft Corporation -- Helicopter Configuration and Propulsion Systems Study Report No. 57-583, (1957)

Part 1. Statistical Weight Analysis

Folder 10

Kellett Aircraft Corporation -- Helicopter - Plastic Fuselage, (1958)

Proposal for Low-Cost Helicopter Construction Using Reinforced Plastics Report No. 124X90-3; Proposal for Reinforced Plastics - Helicopter Fuselage Structure Report No. 141X90-1; and printed matter

Box 6

Helicopter - Two Blade Teetering - Hydrostatic Bearing

Folder 1

Kellett Aircraft Corporation -- Helicopter - Two Blade Teetering, (1945)

Bell Aircraft Corporation Two Blade Rotor Report No. 30-929-123

Folder 2

Kellett Aircraft Corporation -- Helicopter - Two Place, (1957)

Design Study, Army Two-Place Helicopter Report No. 44-177-TC-416

Folder 3

Kellett Aircraft Corporation -- Helicopter - Two Place - Aircraft Design, (1957-1958)

Civilian Specification, Kellett Aircraft Corporation Two-Place Helicopter and technical data

Folder 4

Kellett Aircraft Corporation -- Helicopter - Two Place - Bell, (1957)

Two-Place Observation Helicopter Design Study Summary Report, Report No. D233-099-001

Folder 5

Kellett Aircraft Corporation -- Helicopter - Two Place - Company Sponsored, (1958)

Army Two Place Helicopter K-27; Two-Place Helicopter Development Program for Production; memorandums; and technical data

Folder 6

Kellett Aircraft Corporation -- Helicopter - Two Place - Flying, (1958)

Technical data and printed matter

Folder 7

Kellett Aircraft Corporation -- Helicopter - Two Place - K27 Characteristics, (1958)

Autogiro Characteristics, Two Place Helicopter K-27 Performance, technical data, printed matter, and photographs

Folder 8

Kellett Aircraft Corporation -- Helicopters at Automobile Prices? By Larry M. Hewin, AFIAS U.S. Army Transportation Research Command Fort Eustis, Virginia, (1964)

Included: Letter from Yackle, Albert R. to Larry M. Hewin

Folder 9

Kellett Aircraft Corporation -- Helio - Aircraft, (1957)

Helio Courier Comparative Value Analysis, interoffice memorandum, and printed matter

Folder 10

Kellett Aircraft Corporation -- Hydrostatic Bearing, (1957)

Sikorsky Aircraft Corporation; The Franklin Institute; A New Pressure-Sensing Instrument by Wallace E. Frank and Robert J. Gibson; Bearings for Helicopter Rotor Systems; The Determination of Flow, Film Thickness and Load Carrying Capacity of Hydrostatic Bearings Through the Use of the Electric Analog Field Plotter by Alfred M. Loeb; Hydrostatic Lubrication by Dudley D. Fuller; SAE Aeronautical Information Report No. 47 Fretting; Proposal for Development of Rotor Blade Root Retention System Employing Hydrostatic Lubrication Report No. 150X10-1; photographs; technical data; and correspondence

Box 7

Institute of the Aeronautical Sciences - New Design Data

Folder 1

Kellett Aircraft Corporation -- Institute of the Aeronautical Sciences papers, (1956-1959)

Investigation of the Temperature Distribution and Thermal Stresses in a Hypersonic Wing Structure; Thermal Stresses and Deformations in Beams; VTOL Fixed-Wing Aircraft; Approximate Procedures for Transient Thermal Stresses in Missile Structures; Influence of Aerodynamic Heating on the Effective Torsional Stiffness of Thin Wings; The Effect of Blade Root Properties on the Natural Mode Shapes, Bending Moments, and Shears of a Model Helicopter Rotor Blade; Examination of Some of the Problems Involved in the Design of Propeller-Driven Vertical-Take-Off Transport Airplanes; Reverse Thrust, Vertical Lift, and Side Force by Means of Controlled Jet-Deflection; Helicopter Blade Vibration and Flutter; An Analytical Procedure for the Preliminary Structural and Dynamic Design, and Weight Estimation of Helicopter Rotor Blades; The Flying Platform as a Research Vehicle for Ducted Propellers; Comparison of Current Operational Rotor Systems and a Rotor Having Floating Hub and Offset Coning Hinges; and Sources of Helicopter Development and Manufacturing Costs

Folder 2

Kellett Aircraft Corporation -- Investigation of Airplane Design Requirements with Respect to Reducing Complexity and Cost, (1952)

Folder 3

Kellett Aircraft Corporation -- An Investigation of Creep and Failure of Steel in the Zone of Stress Concentration by Prof. IL. Mirkin and Engineer I.I. Trunin, (1957)

Folder 4

Kellett Aircraft Corporation -- K-27, (1958)

Proposal for Two Place Helicopter K-27 Report No. 124X90-4

Folder 5

Kellett Aircraft Corporation -- Landing Gear Design, (1945)

Consolidated Vultee Aircraft Corporation. Compatibility of Roadability and Landing Requirements in Aircraft Undercarriages by Reinhardt M. Rosenberg

Folder 6

Kellett Aircraft Corporation -- Lifting Systems for VTOL Vehicles Report No. 2, (1959)

Vehicle Research Corporation

Folder 7

Kellett Aircraft Corporation -- LOA Design Data, (1958-1960)

Correspondence, Group Weight Statement, Aerodynamic and Design Evaluation of Results of the Army Two - Place Observation Helicopter Studies, and technical data

Folder 8

Kellett Aircraft Corporation -- MC-4 Helicopter, [undated]

Some Facts About the MC-4 Helicopter

Folder 9

Kellett Aircraft Corporation -- [Miscellaneous], (1949-1957)

American Helicopter Society, Inc. Newsletter Vol 3, No. 6 and American Helicopter Vol. 16, No. 10

Folder 10

Kellett Aircraft Corporation -- [Miscellaneous], [undated]

Twin Anti-Torque Rotors; Drone Characteristics diagrams; and Standby Rocket Engines for Rotary Wing Aircraft

Folder 11

Kellett Aircraft Corporation -- Models for Helicopters, (1953)

On the Design of Models for Helicopter Research and Development Report No. 240

Folder 12

Kellett Aircraft Corporation -- New Design Data, (1954)

New Design Data Index; Evaluation of Casting Process; Stresses in a Ring Loaded Normal to Its Plane; and printed matter

Box 8

One man helicopter - Proceedings of Rotating Wing Aircraft Meeting

Folder 1

Kellett Aircraft Corporation -- One man helicopter, (1955-1957)

KH-15 Helicopter, printed matter, and technical data

Folder 2

Kellett Aircraft Corporation -- Performance Helicopter, (1946-1951)

Helicopter Loading Report No. 1400-24; A Chart Method For Calculating Helicopter Performance - 2 Report No. 130.13; and technical data

Folder 3

Kellett Aircraft Corporation -- Performance Helicopter, (1948-1952)

Effect of Compressibility on Figure of Merit from NACA Full-Scale Tests Report no. XA-102; technical data; and blueprints

Folder 4

Kellett Aircraft Corporation -- Performance Investigation KH-19 Series Report no. 79A-90-1, (1954)

Folder 5

Kellett Aircraft Corporation -- Performance one man helicopter, (1954)

Structural Design Criteria KH-19 Report no. 79S-90-1

Folder 6

Kellett Aircraft Corporation -- Powerplant, Helicopters Auxiliary Power, (1953-1959)

Design Considerations For A Helicopter Gas Turbine Powerplant by J.L. Koetting and Leon R. Wosika; Rotor Speed Control For Free Turbine Engines in Multi-Engine Helicopters by Richard H. Rosenberg and Roland L. Paquette; Some Notes on Helicopter Power Systems by Raymond A. Young, American Helicopter Society; correspondence from Mijanovich, R.T. to Leonard Goland, Amour

Folder 7

Kellett Aircraft Corporation -- Practical Guide on Helicopter Stability, Control and Handling Characteristics, (1960)

Interim Presentation of Results Contract No. DA 44-177-TC-599

Folder 8

Kellett Aircraft Corporation -- Preliminary Rotor Blade Stress Report, (1954)

Kaman Aircraft Corporation Report No. T-73

Folder 9

Kellett Aircraft Corporation -- Proceedings of an N.A.S.A. Briefing on VTOL/STOL Aircraft Research, (1969)

Given at the U.S. Army Transportation Research Command

Folder 10

Kellett Aircraft Corporation -- Proceedings of Rotating Wing Aircraft Meeting at Franklin Institute, (1939)

Institute of the Aeronautical Sciences

Box 9

Proposal. Development of a Rigid Rotor - Stabilization

Folder 1

Kellett Aircraft Corporation -- Proposal. Development of a Rigid Rotor, (1956)

Folder 2

Kellett Aircraft Corporation -- Republic Stress Data, (1946-1954)

Stress and Structures Bulletins Republic Aviation Corporation

Folder 3

Kellett Aircraft Corporation -- Rotor Blade - Stress Analysis, (1940-1954)

Stress Analysis of Rotor Blades: A Summary of Present Practice; A Determination of the Bending Moments In The planes of Rotation of a Constant Rotational Speed Teetering Helicopter Rotor, in Steady Flight Report No. 230.42; Preliminary Stress Analysis Proposed All Metal Blade - XR - 10 Report No. 250.30; Description of Aluminum Allow Rotor Blade As Proposed for XR-10 Job X4687 Report No. 210.8; Preliminary Stress Analysis KH-17A Rotor Blade Report No. 58S-10-2; Design of Rotor Blades Report No. 230.19

Folder 4

Kellett Aircraft Corporation -- Rotor Hoovering Performance, (1954)

Power Loading vs. Disc Loading; Hoovering Performance technical data

Folder 5

Kellett Aircraft Corporation -- Rotor Performance - Propeller Design, (1951-1954)

Propellers for High Powers and Transonic Speeds by George W. Brady; Structural Design of High-Speed Propellers, F.B. Stulen, Propeller Division, Curtiss-Wright Corp.; and technical data

Folder 6

Kellett Aircraft Corporation -- Sandwich Construction, (1951)

United States. Department of Defense. Sandwich Construction for Aircraft, Part 1 and 2

Folder 7

Kellett Aircraft Corporation -- Sikorsky S-62, (1958)

Printed matter

Folder 8

Kellett Aircraft Corporation -- Stabilization - Helicopters, (1959-1961)

The Society of Experimental Test Pilots newsletter; Some Remarks on Dynamic Stability of the Helicopters and Characteristics of Gyratory Stabilizing Systems; A Type of Lifting Rotor with Inherent Stability; An Investigation of the Handling Qualities of a Sikorsky H-19 Helicopter Equipped with Varoius Mechanical Stabilizers Part 2. Flight Test Evaluation of the Optimum Stabilization System; Interim Presentation of Results. A Practical Guide on Helicopter Stab

Box 10

Statistical Survey... - Study of Helicopter Structural Design Criteria

Folder 1

Kellett Aircraft Corporation -- Statistical Survey of Velocities and Accelerations for Field and Carrier Landings of Various Aircraft Report No. 4786, (1952)

The Glenn L. Martin Company

Folder 2

Kellett Aircraft Corporation -- Structural Data Design, (1951-1953)

Engineering Memorandum #10818, Loads Prediction for Structural Rigid Rotor Systems, and technical data

Folder 3

Kellett Aircraft Corporation -- Structural Design Criteria, (1957-1960)

Proposal to Determine a Method for Specifying Design Loads Associated with Flight Maneuver and Skid Landing Maneuver Criteria Report No. 121X90-5; Interim Report Study of Helicopter Structural Design Criteria Report No. 121X90-2; and Helicopter Structural Design Criteria: Analytical Solutions of Flight and Landing Maneuvers

Folder 4

Kellett Aircraft Corporation -- Structures Criteria, (1955-1956)

Comments on Helicopter Design and Test Requirements by Robert H. Lynn and List of NACA Papers on Rotating Wing Aircraft, Part B

Item 5

Kellett Aircraft Corporation -- Structures Manual, (1946)

No folder

Folder 6

Kellett Aircraft Corporation -- Study of Helicopter Structural Design Criteria Report No. 58-336, 1958

Box 11

Technical Data K-25 - YH-32

Folder 1

Kellett Aircraft Corporation -- Technical Data K-25

Proprotor Control; Preliminary Study Blade Pitch Inertia; and technical data

Folder 2

Kellett Aircraft Corporation -- Theory of Rotor Blade Uncoupled Flap Bending Aero-Elastic Vibrations by Peter F. Leone, Chief of Vibrations, (1954)

Folder 3

Kellett Aircraft Corporation -- Transcendental, (1957)

Printed matter and Report No. 1410.1

Folder 4

Kellett Aircraft Corporation -- Transport Helicopter Operating Cost Analysis Methods Report No. 360.1, (1956)

For the United States Army through the Office of Naval Research - Air Branch

Folder 5

Kellett Aircraft Corporation -- Two - Man Cost FST, (1957-1958)

Estimates, Program Comparison, and technical data

Folder 6

Kellett Aircraft Corporation -- VTOL / STOL references, (1950s)

Reports Ordered from ASTIA for K-25 Project and Biography of VTOL and STOL Reports

Folder 7

Kellett Aircraft Corporation -- WADC Rapid Performance Prediction Method for Compound Type Rotorcraft Report No. 55-410, (1959)

Bell Helicopter Corporation

Folder 8

Kellett Aircraft Corporation -- Weight Estimation, (1955)

Wing Weight Estimating Simplified and technical data

Folder 9

Kellett Aircraft Corporation -- Wood Aircraft, (1951)

United States. Department of Defense. Wood Aircraft Inspection and Fabrication and Design of Wood Aircraft Structures

Folder 10

Kellett Aircraft Corporation -- YH-32 (Hiller Ram Jet) Performance, (1951-1958)

American Helicopter Vol. XXI, No. 3 and ARDC YH-32. Limited Performance and Stability

Lockheed Aircraft Corporation

Box 12

1200 lb. - AH-56

Folder 1

Lockheed Aircraft Corporation -- 1200 lb., (1990)

Wing Lower Surface Equivalent Thicknesses; Performance - Option D LRAACA; technical data; and a clipping

Folder 2

Lockheed Aircraft Corporation -- 1989 IRAD Report High Altitude Atmospheric Research Platform (HAARP) Development (U), (1989)

Folder 3

Lockheed Aircraft Corporation -- Advanced Design Subsonic Aircraft, (1986)

Presentation material

Folder 4

Lockheed Aircraft Corporation -- Advanced Ship-Based Aircraft Technologies, (1983)

Independent Research and Development Program Plan Project No. 83011300

Folder 5

Lockheed Aircraft Corporation -- Advanced Ship-Based Multipurpose Aircraft (V/STOL, STO-VL, STO-AL, STOL & CTOL), (1982)

Independent Research and Development Program Plan Project No. 82011300

Folder 6

Lockheed Aircraft Corporation -- Aerocycle, (1962)

Technical data and correspondence

Folder 7

Lockheed Aircraft Corporation -- AH-56, (1971)

Production Cheyenne Producibility / Cost Reduction Study Proposal For Phase 1 Engineering Design Contractor, LR 24301 and Production Cheyenne Producibility / Cost Reduction Study Draft, Description of Work For Phase I Engineering Design Contractor

Folder 8

Lockheed Aircraft Corporation -- AH-56, (1971)

AH-56A, Phase III Configuration, Detail Cost Estimation Analysis

Folder 9

Lockheed Aircraft Corporation -- AH-56, [undated]

Brochure

Folder 10

Lockheed Aircraft Corporation -- AH-56, [undated]

Pictorial Report from Concept to First Flight; Warbird Tech Series: Lockheed AH-56A Cheyenne, Vol. 27; and printed material

Box 13

Aircraft Antisubmarine Warfare... - ASW Development

Folder 1

Lockheed Aircraft Corporation -- Aircraft Antisubmarine Warfare Systems Requirements and Advanced Concepts, (1988)

Presentation material

Folder 2

Lockheed Aircraft Corporation -- Aircraft Conceptual Design, (1984)

Presentation material

Folder 3

Lockheed Aircraft Corporation -- American Institute of Aeronautics and Astronautics, (1968)

Shrouded Propellers - A Comprehensive Performance Study Paper No. 68-994

Folder 4

Lockheed Aircraft Corporation -- American Institute of Aeronautics and Astronautics, (1977)

A Collection of Technical Papers

Folder 5

Lockheed Aircraft Corporation -- American Institute of Aeronautics and Astronautics presentation and charts, (1985)

Presentation material for Modern Aircraft System Design

Folder 6

Lockheed Aircraft Corporation -- Application of the Compound Helicopter, (1972)

Folder 7

Lockheed Aircraft Corporation -- Army Preliminary Evaluation I and Research and Development Acceptance Test I AH-56A Cheyenne Compound Helicopter, (1972)

Folder 8

Lockheed Aircraft Corporation -- ASW Development, (1980-1987)

Looking Beyond the Maritime Strategy; Aircraft Antisubmarine Warfare; Aircraft Antisubmarine Warfare Systems Requirement and Advanced Concepts; Sonar; Three Considerations for Underwater Detection; Submarine Design Considerations: A Compilations of Notes; Evolution of the P-3 Orion Aircraft; The Big Splash; and Elementary Concepts in Underwater Acoustics as Related to Antisubmarine Warfare

Box 14

ASW Lecture - Blowing Effects

Folder 1

Lockheed Aircraft Corporation -- ASW Lecture, (1987-1988)

Systems Requirement and Advanced Concepts Antisubmarine Warfare and Anticraft Antisubmarine Warfare Systems Requirements and Advanced Concepts

Folder 2

Lockheed Aircraft Corporation -- ASW Long Endurance Aircraft, (1982)

Presentation material

Folder 3

Lockheed Aircraft Corporation -- Autogiro Configurations, (1960)

“Skycopter” Is Newest Rotary-Wing Aircraft In Demanding Field, technical notes, blueprints, and photographs

Folder 4

Lockheed Aircraft Corporation -- Autogiro History, (1961)

The Journal of the Royal Aeronautical Society, vol. 65, no. 610. The First Cierva Memorial Lecture. The Era of the Autogiro by J.A.J. Bennett [copies]

Folder 5

Lockheed Aircraft Corporation -- Austere Cheyenne, (1972)

Flyaway Cost Breakdown; interdepartmental communication; Skunk Works Operating Rules; and technical data

Folder 6

Lockheed Aircraft Corporation -- BAFO, [undated]

Presentation material

Folder 7

Lockheed Aircraft Corporation -- Battle Group Passive Horizon Extensive Pylon Design Study, (1981)

Folder 8

Lockheed Aircraft Corporation -- Big Step Presentation (CORLAC), (1963)

The Lockheed Rigid Rotor. A Major Technical Advancement

Folder 9

Lockheed Aircraft Corporation -- Blowing Effects, (1980-1984)

Survey of Spanish Blowing Effects on Aircraft Stability by C.J. Dixon and High-Lift Capability of Low Aspect Ratio Wings Utilizing Circulation Control and Upper Surface Blowing by Roger J. Furey

Box 15

Circulation Control - Composite Aircraft Program

Folder 1

Lockheed Aircraft Corporation -- Circulation Control - A Bibliography of DTNSRDC Research and Selected Outside Reference by Robert J. Englar, (1984)

David W. Taylor Naval Ship Research and Development Center

Folder 2

Lockheed Aircraft Corporation -- CL 660 Mission Potential, (1985)

Presentation material

Folder 3

Lockheed Aircraft Corporation -- Commercial Helicopter Outlook Operational and Mechanical Reliability, (1960)

An Address Before the American Helicopter Society Sixteenth Annual National Forum

Folder 4

Lockheed Aircraft Corporation -- Compass Cope Airframe Design History by Robert Benton Brown, (1980)

Folder 5

Lockheed Aircraft Corporation -- Composite Aircraft for U.S. Navy, (1967)

Folder 6