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Pressure and Heat Transfer Measurements for Hypersonic Flows over Expansion Corners and Ahead of Ramps. Part IV: Mach 8 Heat Transfer Data for Flows Ahead of Ramps: Part of an Investigation of Hypersonic Flow Separation and Control Characteristics

Report Number: ASD TDR 63-679 Part 4
Author: Kaufman, Louis G.
Corporate Author: Grumman Aircraft Engineering Coporation
Laboratory: Air Force Flight Dynamics Laboratory
Date of Publication: 1964-07
Pages: 160
Contract: AF 33(616)-8130
Project: 8219
Task: 821902
AD Number: AD0607038

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