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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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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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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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Thermo-Elastic Stresses And Deflections In Beam-Columns
Author(s): Boley, Bruno A., Mechanic, HaroldCorporate Author(s): Institute Of Air Flight Structures, Columbia University
Laboratory: Aircraft Laboratory
Date of Publication: 1954-03
Report number: WADC TR 54-425
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Thermo-Elastic Stresses And Deflections In Thin-Walled Beams
Author(s): Boley, Bruno A., Tolins, Irwin S.Corporate Author(s): Institute Of Flight Structures, Columbia University
Laboratory: Aircraft Laboratory
Date of Publication: 1954-12
Report number: WADC TR 54-426
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Development Of Equipment For The Experimental Measurement Of The Moments Of Inertia, And Product Of Inertia Of Aircraft
Author(s): Woodward, Claude R.Corporate Author(s): Cornell Aeronautical Laboratory, Inc.
Laboratory: Aircraft Laboratory
Date of Publication: 1954-06
Report number: WADC TR 54-237
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Effects Of Structural Flexibility On Gust Loading Of Aircraft Part II: Dynamic Stresses In Swept-wing Airplanes
Author(s): Kirsch, A. A., Foss, K. A., Calligeros, J. M.Corporate Author(s): Peroelastic And Structures Research Laboratory, Massachusetts Institute Of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1955-08
Report number: WADC TR 54-592 Part 2
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Effects Of Structural Flexibility On Gust Loading Of Aircraft Part I: Gust Loads On Swept-wing Airplanes Free To Pitch And To Deform Statically
Author(s): Foss, K. A.Corporate Author(s): Peroelastic And Structures Research Laboratory, Massachusetts Institute Of Technology
Laboratory: Aircraft Laboratory
Date of Publication: 1955-03
Report number: WADC TR 54-592 Part 1
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