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31 items
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Aerodynamic Noise And The Estimation Of Noise In Aircraft
Author(s): Rogers, Orville R., Cook, Robert F.Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1952-02
Report number: WADC TR 52-341
full text available
New Standard Atmosphere: The WADC 1952 Model Atmosphere
Author(s): Williams, D. T., Nash, W. F., Bell, J. C.Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1954-03
Report number: WADC TR 54-215
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Theoretical Investigation Of Optimum Pressures In Aircraft Hydraulic Systems
Author(s): Cooke, Conrad H., Smith, Robert L. , Gessner, EugeneCorporate Author(s): Glenn L. Martin Company
Laboratory: Aircraft Laboratory
Date of Publication: 1954-01
Report number: WADC TR 54-189 Volume 1
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Theoretical Investigation Of Optimum Pressures In Aircraft Hydraulic Systems
Author(s): Cooke, Conrad H., Smith, Robert L., Martin, Glenn L., Gessner, EugeneCorporate Author(s): Glenn L. Martin Company
Laboratory: Aircraft Laboratory
Date of Publication: 1954-01
Report number: WADC TR 54-189 Volume 2
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Flutter Characteristics Of Low Aspect Ratio wings In Incompressible Flow. Part I: Development Of The Basic Theory Of The Method
Author(s): Lawrence, H. R., Stone, H. N.Corporate Author(s): Cornell Aeronautical Laboratory, Inc.
Laboratory: Aircraft Laboratory
Date of Publication: 1957-05
Report number: WADC TR 54-412 Part 1
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Three-dimensional Supersonic Flutter Model Tests Near Mach Number 1.5. Part 1: Model Design And Testing Techniques
Author(s): McCarthy, John F., Jr., Prigge, John S., Jr., Levy, Gilbert M., Asher, Gifford W.Corporate Author(s): Aeroelastic And Structures Research Laboratory, Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1955-12
Report number: WADC TR 54-113 Part 1
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Shock-Tube Flow Investigations. Part 1. An Exploratory Study Of The Generation Of Blast-Type Profiles In The Shock Tube By The Reflection Method
Author(s): Lee, Robert C. K., Witmer, Emmett A., Ruetenik, J . RayCorporate Author(s): Massachusetts Institute of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1956-08
Report number: WADC TR 54-383 Part 1
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Analytical Studies Of Aircraft Structures Exposed To Transient External Heating Volume III Thermal Response Of The Skin And Support Flange Of A Structural Joint
Author(s): Ambrosio, Alphonso, Ishimoto, TakaoCorporate Author(s): University 0f California, Department Of Engineering
Laboratory: Aircraft Laboratory
Date of Publication: 1955-01
Report number: WADC TR 54-579 Volume 3
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Analytical Studies Of Aircraft Structures Exposed To Transient External Heating Volume IV Heat-Transfer Coefficients For Speeds Up To M-3, With Emphasis On Effects Of Wall-Temperature Variations
Author(s): Knuth, Eldon L., Bussell, BertramCorporate Author(s): University 0f California, Department Of Engineering
Laboratory: Aircraft Laboratory
Date of Publication: 1957-09
Report number: WADC TR 54-579 Volume 4
full text available
Testing Of Metal Boss Seals
Author(s): Kupiec, Harry P.Corporate Author(s): Aircraft Equipment Testing Co.
Laboratory: Aircraft Laboratory
Date of Publication: 1955-04
Report number: WADC TR 55-163
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