DocumentCode :
2941568
Title :
Non-isentropic effects on the WRDC 20 inch hypersonic wind tunnel calibration
Author :
Buck, Melvin L. ; Draper, Alfred C.
Author_Institution :
Wright Res. & Dev. Center, Wright-Patterson AFB, OH, USA
fYear :
1989
fDate :
18-21 Sep 1989
Firstpage :
19
Lastpage :
28
Abstract :
An experiment was conducted in the Wright Research and Development Center 20-in. hypersonic wind tunnel to assess nonisentropic effects on the test section Mach number. Pressure measurements were made on a blunt 5° cone. These pressures were then compared with a parabolized Navier-Strokes code to define the free-stream Mach number. The results indicate that the nonisentropic effects are not significant. There is no pronounced difference in the Mach number from that determined by the more conventional Pitot pressure probe survey
Keywords :
calibration; hypersonic flow; pressure measurement; wind tunnels; 20 inch; WRDC; calibration; free-stream Mach number; hypersonic wind tunnel; nonisentropic effects; parabolized Navier-Strokes code; pressure measurement; Calibration; Character generation; Computational fluid dynamics; Petroleum; Pollution measurement; Pressure measurement; Probes; Reservoirs; Temperature; Testing;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Instrumentation in Aerospace Simulation Facilities, 1989. ICIASF '89 Record., International Congress on
Conference_Location :
Gottingen
Type :
conf
DOI :
10.1109/ICIASF.1989.77655
Filename :
77655
Link To Document :
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