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PRESSURE AND HEAT TRANSFER MEASUREMENTS FOR HYPERSONIC FLOWS OVER EXPANSION CORNERS AND AHEAD OF RAMPS. PART 3: MACH 8 PRESSURE DATA FOR FLOWS AHEAD OF RAMPS PART OF AN INVESTIGATION OF HYPERSONIC FLOW SEPARATION AND CONTROL CHARACTERISTICS [report]

II Kaufman, Louis G.
1963 unpublished

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Pressure and heat transfer data were obtained for hypersonic flows over 40-degree expansion corners and ahead of ramps. Full and partial span ramps, having wedge angles up to 90 degrees, were tested at two locations on a sharp leading edge flat plate, with and without end plates. Pressure data were obtained for M = 5 00 ,for model length Rejmolds numbers between 1.1 and 6.6 million. Both pressure and heat transfer data were obtained for M = 8 * 00 for Rejmiolds numbers between 1.1 and 3.3
more » ... n. PUBLICATION REVIEW This report has been reviewed and is approved.
doi:10.21236/ad0431202 fatcat:6cdzrnwcrrahlnql4vr5k7xtpq
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II Kaufman, Louis G.. "PRESSURE AND HEAT TRANSFER MEASUREMENTS FOR HYPERSONIC FLOWS OVER EXPANSION CORNERS AND AHEAD OF RAMPS. PART 3: MACH 8 PRESSURE DATA FOR FLOWS AHEAD OF RAMPS PART OF AN INVESTIGATION OF HYPERSONIC FLOW SEPARATION AND CONTROL CHARACTERISTICS." (1963)