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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., II
Corporate 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., II
Corporate 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., II
Corporate 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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Aircraft Motion Analysis
Author(s): Thelander, J. A.
Corporate Author(s): Douglas Aircraft Company
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-03
Report number: FDL TDR 64-70
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Theoretical Investigations of Boundary Layer Stability
Author(s): Raetz, Gibbs S., Brown, W. Byron
Corporate Author(s): Northrop Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1966-09
Report number: AFFDL TR 64-184
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Active Control of Booster Elasticity
Author(s): Swaim, Robert L.
Corporate Author(s): Air Force Flight Dynamics Laboratory
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-04
Report number: AFFDL TR 64-189
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Response of Elastic Structures to Deterministic and Random Excitation
Author(s): Barnoski, R. L.
Corporate Author(s): Measurement Analysis Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1965-05
Report number: AFFDL TR 64-199
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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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