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Pressure and Heat Transfer Measurements at Mach 13 and 19 for Flows Ahead of Ramps, Over Expansion Corners, and Past Fin-Plate Combinations: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Hatofilis, Stavros A.
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-09
Report number: FDL TDR 64-144
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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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Pressure and Heat Transfer Measurements for Mach 8 Flows Over a Blunt Pyramidal Configuration with Aerodynamic Controls: Part II" Pressure 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 Engineering Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-09
Report number: FDL TDR 64-2 Part 2
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Static Aerodynamic Characteristics at Mach 5 and 8 of an Aerodynamically Controllable Winged Re-Entry Configuration. Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Meckler, Lawrence
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Report number: FDL TDR 64-10
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Pressure and Heat Transfer Measurements for Flows Ahead of Ramps Part III: Mach 8 Pressure 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 Corporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1963-12
Report number: ASD TDR 63-679 Part 3
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Pressure and Heat Transfer Measurements for Hypersonic Flows over Expansion Corners and Ahead of Ramps Part II: Mach 5 Pressure 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 Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Report number: ASD TDR 63-679 Part 2
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Pressure and Heat Transfer Measurements for Hypersonic Flows over Expansion Corners and Ahead of Ramps Part I: Mach 5 and 8 Data for Expansion Corner Flows: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Kaufman, Louis G.
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Report number: ASD TDR 63-679 Part 1
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Pressure Measurement at Mach 19 for a Winged Re-Entry Configuration: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Hartofilis, Stavros A.
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Flight Control Division
Date of Publication: 1963-05
Report number: ASD TDR 63-319
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Pressure Distributions and Oil Film Photographs for Mach 5 Flows Past Fins Mounted on a Flat Plate: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Kaufman, Louis G.
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Report number: ASD TDR 63-755
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Experimental Investigation of Pressures on a Blunt Two-Dimensional Profile and on Sharp and Blunt Conical Shapes of Noncircular Cross Section at Mach 5 and 8
Author(s): Mead, Harold R., Koch, Frank
Corporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Flight Control Laboratory
Date of Publication: 1963-08
Report number: ASD TDR 63-169

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