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Pressure Measurements at Mach 8 on an Aerodynamically Controllable Winged Re-Entry Configuration: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Meckler, LawrenceCorporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1965-06
Report number: FDL TDR 64-124
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Heat Transfer Measurements at Mach 9 on an Aerodynamically Controllable Winged Re-Entry Configuration: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics
Author(s): Meckler, LawrenceCorporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1964-09
Report number: FDL TDR 64-142
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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, LawrenceCorporate 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 at Mach 5 and 8 for a Fin-Flat Plate Model: Part of an Investigation of Hypersonice Flow Separation and Control Characteristics
Author(s): Kaufman, Louis G., Meckler, LawrenceCorporate Author(s): Grumman Aircraft Engineering Corporation
Laboratory: Flight Control Laboratory
Date of Publication: 1963-04
Report number: ASD TDR 63-235
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