Investigation on transonic convex-corner flows

研究成果: Article同行評審

26 引文 斯高帕斯(Scopus)

摘要

An experimental investigation was conducted to study the transonic flow past convex corners. The mean surface pressure indicated strong inviscid-viscous interactions, and the interaction region increased with the freestream Mach number and the convex-corner angle. Unsteadiness of the interaction was characterized by an intermittent region and a local peak pressure fluctuation. The peak pressure fluctuations and the tentative boundary between the attached and separated flows could be scaled with the convex-corner angle and a second-order freestream Mach number (M2η).

原文English
頁(從 - 到)1014-1018
頁數5
期刊Journal of Aircraft
39
發行號6
DOIs
出版狀態Published - 2002

All Science Journal Classification (ASJC) codes

  • 航空工程

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