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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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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., II
Corporate 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., 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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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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Pressure and Heat Transfer Measurements fro Mach 21 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls
Author(s): Kaufman, Louis G., II
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-08
Report number: FDL TDR 64-120
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Pressure Measurements For Mach 8 Flows Over Expansion Corners And Ramps On An Internally Cooled Model. Part II. Flows Over A Flat Plate With And Without A Partial Span Ramp.
Author(s): Kaufman, Louis G., II
Corporate Author(s): Grumman Aircraft Engineering Corp Bethpage N Y
Date of Publication: 1964-10
Report number: RTD TDR 63-4044 Part 2
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Pressure Measurements For Mach Five Flows Over Winged Re-Entry Configurations With Aerodynamic Controls. Part I. Blunt Cabin Configuration
Author(s): Kaufman, Louis G., II
Corporate Author(s): Grumman Aircraft Engineering Corp Bethpage N Y
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-02
Report number: RTD TDR 63-4179 Part 1
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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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Pressure Measurements for Mach 8 Flows Over Expansion Corners and Ramps on an Internally Cooled Model Part III. Flows Over Full Span Ramps Mounted on a Flat Plate
Author(s): Kaufman, Louis G., II
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-05
Report number: RTD TDR 63-4044 Part 3

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