Transonic cavity-convex corner interactions

研究成果: Article同行評審

2 引文 斯高帕斯(Scopus)

摘要

An experimental study was conducted to investigate the transonic convex-corner flows with and without the presence of an upstream cavity. Measurements were made to investigate the geometric effect and the spacing of a cavity on attached and separated convex-corner flows. The upstream expansion and downstream initial recompression are strongly affected by the upstream cavity, which includes the delay on the transition of subsonic and transonic expansion flows, the initial boundary-layer separation, the characteristics of separated flow, and the intensity of surface pressure fluctuations.

原文English
頁(從 - 到)1131-1136
頁數6
期刊Journal of Aircraft
40
發行號6
DOIs
出版狀態Published - 2003

All Science Journal Classification (ASJC) codes

  • 航空工程

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