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

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

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Provenance: AFRL/VACA

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