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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

Report Number: ASD TDR 63-679 Part 1
Author(s): Kaufman, Louis G.
Corporate Author: Grumman Aircraft Engineering Corporation
Laboratory: AF Flight Dynamics Laboratory
Date of Publication: 1963-09
Pages: 81
Contract: AF 33(616)-8130
Project: 8219
Task: 821902
AD Number: AD0423580

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