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Upstream blowing jet on transonic convex-corner flow

Authors :
Chung, Kung-Ming
Source :
Journal of Aircraft. Nov-Dec, 2007, Vol. 44 Issue 6, p1948, 6 p.
Publication Year :
2007

Abstract

The present study investigates the effects of an upstream blowing jet on the compressible convex-corner flows. The characteristics of mean and fluctuating pressure distributions are associated with the type of expansion flows, blowing rates, and porosity. Even a small amount of upstream blowing tends to delay the transition of subsonic and transonic expansion flows, thus reducing the levels of downstream surface pressure fluctuations in subsonic interactions. The intensity of surface pressure fluctuations is associated with blowing rates for the separated flows. Larger blowing rates result in upstream movement of shock wave and enhance the flow unsteadiness (or peak surface pressure fluctuations) near the corner. DOI: 10.2514/1.32203

Details

Language :
English
ISSN :
00218669
Volume :
44
Issue :
6
Database :
Gale General OneFile
Journal :
Journal of Aircraft
Publication Type :
Academic Journal
Accession number :
edsgcl.172777565