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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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An Investigation of Hypersonic Flow Separation and Control Characteristics

Author(s): Kaufman, Louis G., II, Meckler, Lawrence, Hartofilis, Stavros A., Weiss, Daniel
Corporate Author(s): Grumman Aircraft Engineerign Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-01

Report number: AFFDL TR 64-174

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Unsteady Aerodynamics for Advanced Configurations: Part V - Unsteady Potential Flow Around Slender Bodies at Angles of Attack

Author(s): Li, T. C.
Corporate Author(s): North American Aviation, Incorporated
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-05

Report number: FDL TDR 64-152 Part 5

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Unsteady Aerodynamics for Advanced Configurations: Part IV - Application of the Supersonic Mach Box Method to Intersecting Planar Lifting Surfaces

Author(s): Moore, M. T., Andrew, L. V.
Corporate Author(s): North American Aviation, Incorporated
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-05

Report number: FDL TDR 64-152 Part 4

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Unsteady Aerodynamics for Advanced Configurations: Part II - A Transonic Box Method for Planar Lifting Surfaces

Author(s): Rodemich, E. R., Andrew, L. V.
Corporate Author(s): North American Aviation, Incorporated
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-05

Report number: FDL TDR 64-152 Part 2

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Unsteady Aerodynamics for Advanced Configurations: Part I - Application of the Subsonic Kernel Function to Nonplanar Lifting Surfaces

Author(s): Vivian, H. T., Andrews, L. V.
Corporate Author(s): North American Aviation, Incorporated
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-05

Report number: FDL TDR 64-152 Part 1

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