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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 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 I. Expansion Corner Flows. Part Of An Investigation Of Hypersonic Flow Separation And Control Characteristics
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: 1963-10
Report number: RTD TDR 63-4044 Part 1

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