Upstream blowing jet on transonic convex-corner flow

研究成果: Article同行評審

5 引文 斯高帕斯(Scopus)

摘要

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.

原文English
頁(從 - 到)1948-1953
頁數6
期刊Journal of Aircraft
44
發行號6
DOIs
出版狀態Published - 2007

All Science Journal Classification (ASJC) codes

  • 航空工程

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