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Stress Analysis of a Parachute During Inflation and at Steady State
Author(s): Heinrich, Helmut G., Jamison, Lelan R., Jr.
Corporate Author(s): University of Minnesota
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-02
Report number: FDL TDR 64-125
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Transducers for Sonic Fatigue Measurements
Author(s): Kelly, Ronald D.
Corporate Author(s): Measurement Analysis Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-02
Report number: AFFDL TR 64-171
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A Conical Thin-Shock-Layer Theory Uniformly Valid in the Entropy Layer
Author(s): Melnik, Robert E.
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-01
Report number: FDL TDR 64-82
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Nonlinear Thermoelasitc Effects on Hypersonic Stability and Control, Part III: Simulation, Measurement and Analysis of Nonlinear Static Aerothermoelastic Behavior of a 45 Degree Delta Wing
Author(s): Batt, James R.
Corporate Author(s): Bell Aerosystems Co.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-02
Report number: FDL TDR 64-16 Part 3
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Transient Dynamic Response of Orbiting Space Stations
Author(s): Tai, C. L., Andrew, L. V., Loh, M. M. H., Kamrath, P. C.
Corporate Author(s): North American Aviation, Incorporated
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-02
Report number: FDL TDR 64-25
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Investigation Of Propellant Actuated Devices For Use In Emergency Crew Escape Systems For Advanced Aerospace Vehicles. Phase III. Design Study.
Author(s): Bleikamp, R. H., Lake, E. R., McGovern, D. R.
Corporate Author(s): McDonnell Aircraft Corp St Louis MO
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-04
Report number: AFFDL TR 65-26 Part 2
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Development Of Aircraft Shock Absorbers Using Friction As The Energy Dissipator
Author(s): Fricker, Walter W.
Corporate Author(s): Cleveland Pneumatic Co OH
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-10
Report number: AFFDL TR 65-96
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An Experimental and Analytical Investigation of Hypersonic Inlet Boundary Layers
Author(s): Stroud, J. F., Miller, L. D.
Corporate Author(s): Lockheed-California Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-08
Report number: AFFDL TR 65-123 Volume 2
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General Instability of Orthotropically Stiffened Cylinders. Part 1. Axial Compression, Torsion and Hdyrostatic Pressure Loadings
Author(s): Milligan, Roger, Gerard, George, Lakshmikantham, C., Becker, Herbert
Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-07
Report number: AFFDL TR 65-161 Part 1
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General Instability of Orthotropically Stiffened Cylinders. Part 2. Bending and Combined Compression and Bending.
Author(s): Lakshmikantham, C., Gerard, George, Milligan, Roger
Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-08
Report number: AFFDL TR 65-161 Part 2

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