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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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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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Six-Degree-of-Freedom Flight Path Study Generalized Computer Program: Part II, Volume 2 - User's Manual for Part I, Volume 2
Author(s): Harris, J. L., Shilling, J. A., Vorwald, R. F.Corporate Author(s): McDonnell Aircraft Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-10
Report number: FDL TDR 64-1 Part 2 Volume 2
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Development of an Advanced Digital Adaptive Flight Control System
Author(s): Zaborszky, J., Luedde, W. J., Berger, R. L., Berger, J. B., Madonna, M. A.Corporate Author(s): McDonnell Aircraft Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-12
Report number: FDL TDR 64-115
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Thermal Response in Sandwich Panels
Author(s): Kendall, P.Corporate Author(s): Martin Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-10
Report number: FDL TDR 64-135
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Unsteady Aerodynamics for Advanced Configurations: Part III - Elliptic-Conical Wing in Linearized Unsteady Transonic Flow
Author(s): Albano, E., 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 3
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Dynamics of Shell-Like Lifting Bodies: Part I. The Analytical Investigation
Author(s): Hung, F. C.Corporate Author(s): North American Aviation, Incorporated
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-06
Report number: AFFDL TR 65-17 Part 1
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A Study of Time-Optimal Rendezvous in Three Dimensions, Volume I
Author(s): Paiewonsky, B. H., Woodrow, P. J.Corporate Author(s): Aeronautical Research Associates of Princeton, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-01
Report number: AFFDL TR 65-20 Volume 1
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Pressure and Heat Transfer Measurements for Hypersonic Flows over Expansion Corners and Ahead of Ramps. Part IV: Mach 8 Heat Transfer 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 Coporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-07
Report number: ASD TDR 63-679 Part 4
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Pressure Measurements For Mach Five Flows Over Winged Re-Entry Configurations With Aerodynamic Controls. Part II. Conical Cabin Configuration
Author(s): Kaufman, Louis G., IICorporate Author(s): Grumman Aircraft Engineering Corp Bethpage N Y
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-02
Report number: RTD TDR 63-4179 Part 2
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