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Ney (Alfred) Personal Papers
SDASM.SC.10231  
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Table of contents What's This?

 

SERIES I: Documents

 

Folder 1 – Newsletter and Articles Includes bulletins from Machine Design, 1958-59.

 

Folder 2 – San Diego Aircraft Engineering Employee Handbook

 

Folder 3 – Personal Notes Consists of a handwritten timeline, 1947-48.

 

Folder 4 – Spiral Notebooks Personal notes continued.

 

Folder 5 – Technical Memorandums Three memorandums, 1947-48.

 

Folder 6 – Weekly Reports 5 reports, 1947-48.

 

Folder 7 – Cooling/ Exhaust/ Air Conditioning Documents

 

Folder 8 – Loose Manual Pages Includes 5 pages of ‘Rivet

 

Folder 9 – XP-92/Offenhauser Engine Documents

 

Folder 10 – Miscellaneous Documents

 

SERIES II: Reports

 

Folder 11 – Reports prepared by A.M. Ney

Physical Description: “Reliability Test Outline for the Valve, Fuel, Staging Disconnect Shut-off”; GD Convair, 10 Oct. 1960; “Specific Test Conditions for the Fuel Fill and Drain Rise-off,” GD Convair, 22 March 1961.
 

Folder 12 – The Fundamentals of Flight-Induced and Forced Cooling by J.H. Browster, III

 

Folder 13 – High Altitude Auxiliary Power Unit Development by H.F. Dunholter

 

Folder 14 – Estimating Reliability by Test-to-Failure Report 2X-7-014, 30 June 1956

 

Folder 15 – Elements of Fluid Mechanics, Nov. 1962-March 1963

 

Folder 16 – Convair Astronautics Design Manual Section 1, Ch. 2 Human Engineering, 3 March 1961

 

Folder 17 – A.P.U. Vibration Analysis for XP-92, 24 May 1948

 

Folder 18 – Report on Offenhauser Tests for January-June 1948 (2 copies)

 

Folder 19 – Nuclear Powered Flight Progress Report, John Hopkins University, 14 Jan. 1947

 

Folder 20 – Estimating Reliability by Attribute Testing Report ZX-7-011, 21 Nov. 1955

 

Folder 21 – Report on Paint Stripping and Cleaning Compounds for Aircraft USES-Investigation of “Madaco Sol Oil” “G-BEX-D”, and “Ameroid Duosol” Degreasing Compounds, 8 May 1945

 

Folder 22 – Methods for Estimating Pressure Losses in Ducts. Report No. R-109, 26 Feb. 1942

 

Folder 23 – Fundamentals of Probability and Statistics with Reliability Applications Report ZX-7-012, 25 Feb. 1956

 

Folder 24 – Airfoil Section Data Obtained in the N.A.C.A. Variable-Density Tunnel as Affected by Support Interference and other Corrections Report No. 669, 1939

 

Folder 25 – An Investigation of Aircraft Heaters XVIII, A Design Manual for Exhaust Gas and Air Heat Exchangers, August 1945

 

Folder 26 – A Proposal for Cryogenic Insulation Research Volume 1 Technical and Management Report No. GD/A-DDB64-009, 10 April 1964

 

Folder 27 – Analysis of Aircraft Ejector Cooling Performance Report R-447-A, 30 October 1945

 

Folder 28 – German Radiator and Oil-Cooler Construction Project No. DP-156, Sept. 1947

 

Folder 29 – A Theoretical and Experimental Investigation of Exhaust Ejectors for Cooling at Low Speeds, July 1943

 

Folder 30 – An Experimental Investigation of Rectangular Exhaust-Gas Ejectors Applicable for Engine Cooling ARR No. E4E31, May 1944

 

Folder 31 – Research and Development of Inserted Instruments and Materials for High Temperature Measurements in Ramjet Exhausts USCAL Rept. 4-4, 23 May 1947

 

Folder 32 – The Fundamentals of Cooling Power for Incompressible Flow from Momentum Theory Report R-143-E

 

Folder 33 – Airesearch Oil Coolers Performance and Selection Catalog No. LM-2, 2 July 1945

 

Folder 34 – Preknock Vibrations in a Spark-Ignition Engine Cylinder as Revealed by High-Speed Photography Report No. 785, 1944

 

Folder 35 – Ground Tests of Exhaust Gas Thrust Augmenters Report R-50, 20 November 1940

 

Folder 36 – Comparison of Exhaust Jet Propulsion and Supercharger Systems at Military and Cruising Power Report R-65, 7 April 1941

 

Folder 37 – Exhaust Ejector Tests On a Single Cylinder R-2800 Engine Report R-309-B, 12 July 1943

 

Folder 38 – An Experimental Investigation of the Design Variables for NACA Submerged Duct Entrances RM No. A7I30, 8 Jan. 1948

 

Folder 39 – Tests of an Annular Ejector System for Cooling Aircraft Engines ACR No. 3J27, October 1943

 

Folder 40 – The Effect of Exhaust-Stack Shape On the Design and Performance of the Individual Cylinder Exhaust-Gas Jet-Propulsion System, November 1942

 

Folder 41 – Design of Nozzles for the Individual Cylinder Exhaust Jet Propulsion System, April 1941

 

Folder 42 – Tests of Exhaust Propulsion Nozzles Report 3E21, May 1943

 

Folder 43 – Convair Very High Altitude Auxiliary Power Unit Development Report ZK-115-032, 2 August 1948

 

Folder 44 – Convair Propulsion Laboratory Report ZK-002, 2 August 1948

 

SERIES III: Drawings

 

Folder 45 – Model X Underwing Nacelle

Physical Description: 1.P&WA JT9D-1. 2. GE CTF39.
 

Folder 46 – Convair Model 30, 1/50 scale model

 

Folder 47 – Engines (General)

Physical Description: Includes Offenhauser; horse power correction factors; power plant test stand; engine data C-75, Series 13; nose gear switch, jet pump; single engine installation; cooling flower, Lawrence Engr & Research; integrated bleed air anti-icing & A/C system, Tokken F-28.
 

Folder 48 – Miscellaneous Drawings

Physical Description: Includes shear web hole reinforcement; instrumentation schematic; general arrangement model P; Meyer & Drake Dyno set-up; plaster pattern; nomenclature (2 copies); nomenclature wing-general cutaway (2 copies).
 

SERIES IV: Photographs

 

Folder 49 – Photographs Thirteen Convair B&W photographs.