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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., II
Corporate 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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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., II
Corporate 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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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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Design of Linear Flight Control Systems Using Optimal Control Theory
Author(s): Rynaski, E. G., Reynolds, P. A., Shed, W. H.
Corporate Author(s): Cornell Aeronautical Laboratory, Inc.
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-04
Report number: ASD TDR 63-376

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