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,

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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

Author(s):
Kaufman, Louis G., Ii.
Author Organization(s):
GRUMMAN AIRCRAFT ENGINEERING CORP BETHPAGE N Y
Supplementary Note:
A portion of the original document contains fine detail which make reading of photocopy difficult. See also AD-601 805.
Annotation:
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.
Pagination:
0141

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
ASD-TDR63 679 P4
Task Number(s):
821902
Project Number(s):
8219
Monitor Series:
TDR63 679 P4
 Subject Terms
Modernization Areas:
Hypersonics
Communities of Interest:
No COI(s) Identified
Descriptor(s):
(*HYPERSONIC FLOW, HEAT TRANSFER), (*HEAT TRANSFER, HYPERSONIC FLOW), PRESSURE, FLAT PLATE MODELS, WIND TUNNELS, AERODYNAMIC HEATING, HYPERSONIC CHARACTERISTICS, AERODYNAMIC CONTROL SURFACES, EXPERIMENTAL DATA, GRAPHICS
Report Date:
1964 Jul 01