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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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Permanent Buckling Of Sheet-Stringer Panels At Elevated Temperatures
Author(s): Needham, Robert A.
Corporate Author(s): University Of California, Department Of Engineering
Laboratory: Aircraft Laboratory
Date of Publication: 1953-07
Report number: WADC TR 53-209
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Temp-Tapes: Improved Design, Construction, And Calibration
Author(s): Ambrosio, Alphonso, Busseli, Bertram
Corporate Author(s): University Of California, Department Of Engineering
Laboratory: Aircraft Laboratory
Date of Publication: 1953-07
Report number: WADC TR 53-211
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An Experimental Investigation Of Hot Gas Ejectors For Boundary Layer Control
Author(s): De Leo, Richard V.
Corporate Author(s): Rosemount Aeronautical Laboratories, University of Minnesota
Laboratory: Aircraft Laboratory
Date of Publication: 1953-12
Report number: WADC TR 52-128 Part 2
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Theoretical Investigation Of Optimum Pressures In Aircraft Hydraulic Systems
Author(s): Cooke, Conrad H., Smith, Robert L. , Gessner, Eugene
Corporate 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, Eugene
Corporate 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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Method For Predicting Dynamic Landing Loads
Author(s): Eisenman, Richard L., Kramer, Edward H.
Corporate Author(s): Aircraft Laboratory
Laboratory: Aircraft Laboratory
Date of Publication: 1954-09
Report number: WADC TR 54-28
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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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An Investigation Of The Experimental Determination Of Aircraft Inertia
Author(s): Woodard, Claude R.
Corporate Author(s): Cornell Aeronautical Laboratory, Inc.
Laboratory: Aircraft Laboratory
Date of Publication: 1953-07
Report number: WADC TR 53-207

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