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31 items
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Fixed-Base and In-Flight Simulations of Longitudal and Lateral-Directional Handling Qualities for Piloted Re-Entry Vehicles
Author(s): Kidd, Edwin A., Harper, Robert P., Jr.Corporate Author(s): Cornell Aeronautical Laboratory, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-02
Report number: ASD TDR 61-362
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Research and Development of a Hot Gas Flight Stabilization System
Author(s): Feucht, R. E., Taplin, L. B., Bosworth, R., Gregory, A., MacArthur, G.Corporate Author(s): Bendix Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-02
Report number: WADD TR 60-449 Part IV
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Six-Degree-of-Freedom Flight-Path Study Generalized Computer Program: Part I. Problem Formulation
Author(s): Brown, Robert C., Brulle, Robert V., Combs, A. E., Griffin, Gerald D.Corporate Author(s): McDonnell Aircraft Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-10
Report number: FDL TDR 64-1 Part 1 Volume 1
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Pressure Measurements for Mach Five Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Kaufman, Louis G., IICorporate Author(s): Grumman Aircraft Engineerign Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-01
Report number: RTD TDR 63-4239
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Pressure and Heat Transfer Measurements for Mach 8 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls: Part I: Pressure Data for Delta Wing Surface
Author(s): Kaufman, Louis G., IICorporate Author(s): Grumman Aircraft Engineerign Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-01
Report number: FDL TDR 64-2 Part 1
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Pressure and Heat Transfer Measurements for Mach 8 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls: Part III: Heat Transfer Data for Delta Wing Surface
Author(s): Kaufman, Louis G., IICorporate Author(s): Grumman Aircraft Engineerign Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-05
Report number: FDL TDR 64-2 Part 3
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Pressure and Heat Transfer Measurements for Mach 8 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls: Part IV: Heat Transfer Data for Dihedral Surfaces Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Kaufman, Louis G., IICorporate Author(s): Grumman Aircraft Engineerign Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-05
Report number: FDL TDR 64-2 Part 4
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A Survey of Aerodynamic Noise
Author(s): Ingram, J. D.Corporate Author(s): General Technology Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-12
Report number: FDL TDR 64-132
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Theoretical Studies of Methods of Generating Random Waves from Harmonic Sources
Author(s): Samuels, J. C.Corporate Author(s): General Technology Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-12
Report number: FDL TDR 64-133
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Aerodynamic Characteristics and Flap Loads for a Blunt Pyramidal Configuration at Mach 5 and 8: :Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Evans, William J., Kaufman, Louis G., IICorporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-09
Report number: FDL TDR 64-128
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