An Experimental Investigation of Shock-Wave Boundary-Layer Interaction in Hypersonic Flow
نویسندگان
چکیده
منابع مشابه
Experimental Investigation of Shock-Wave/Boundary- Layer Interactions Over an Artificially Heated Model in Hypersonic Flow
Experimental tests have been carried out to analyze the effect of wall-to-total temperature ratio on the characteristics of a fully laminar shock-wave/boundary-layer interaction in a Mach 6 high enthalpy flow. Test cases were run in a new high-enthalpy arc-heated wind tunnel developed at Centrospazio in the framework of the ESA/FESTIP program. In order to heat-up the model surface a high temper...
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ژورنال
عنوان ژورنال: Journal of the Visualization Society of Japan
سال: 1999
ISSN: 1884-037X,0916-4731
DOI: 10.3154/jvs.19.supplement2_267