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Accession Number:
AD0607038
Title:
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,
Corporate Author:
GRUMMAN AIRCRAFT ENGINEERING CORP BETHPAGE N Y
Report Date:
1964-07-01
Abstract:
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 for model length Reynolds numbers between 1.1 and 6.6 million. Both pressure and heat transfer data were obtained for M 8 for Reynolds numbers between 1.1 and 3.3 million. Author
Supplementary Note:
A portion of the original document contains fine detail which make reading of photocopy difficult. See also AD-601 805.
Pages:
0141
File Size:
0.00MB
