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Pressure Measurements For Mach 8 Flows Over Expansion Corners And Ramps On An Internally Cooled Model. Part I. Expansion Corner Flows. Part Of An Investigation Of Hypersonic Flow Separation And Control Characteristics
Author(s): Kaufman, Louis G., II
Corporate Author(s): Grumman Aircraft Engineering Corp Bethpage N Y
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1963-10
Report number: RTD TDR 63-4044 Part 1
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Pressure and Heat Transfer Measurements for Flows Ahead of Ramps Part III: Mach 8 Pressure Data for Flows Ahead of Ramps: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Kaufman, Louis G.
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1963-12
Report number: ASD TDR 63-679 Part 3
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Functional Capability of Neuromime Networks for Use in Attitude Stabilization Systems
Author(s): Lee, R. J., Snyder, R. F.
Corporate Author(s): Adaptronics, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1963-09
Report number: ASD TDR 63-549
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Approximate Methods of Simulating Random Noise with Pure Tone Sources
Author(s): Thiel, C. C.
Corporate Author(s): General Technology Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-12
Report number: FDL TDR 64-131
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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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A Closed-Form Solution to Lifting Reentry
Author(s): Bell, Roland N.
Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-01
Report number: AFFDL TR 65-65
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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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