Investigation on separated and unseparated transonic convex-corner flows

研究成果: Paper同行評審

摘要

A naturally developed turbulent boundary layer past convex comers was studied. Mean surface pressure in Mach 0.64 and 0.83 indicated strong inviscid-viscous interactions. Interaction region increased with Mach number and convex-comer angle. Also, unsteadiness of the interactions was characterized by an intermittent region and local peak pressure fluctuation, which was due to the amplification of lower frequency components as shown in power spectra. At higher convex-comer angle (M = 0.83 and α = 15°) the boundary layer was separated. Unsteady shock motion induced intense surface pressure fluctuation which spectrum was centered at about 780 Hz.

原文English
出版狀態Published - 2000 十二月 1
事件38th Aerospace Sciences Meeting and Exhibit 2000 - Reno, NV, United States
持續時間: 2000 一月 102000 一月 13

Other

Other38th Aerospace Sciences Meeting and Exhibit 2000
國家United States
城市Reno, NV
期間00-01-1000-01-13

All Science Journal Classification (ASJC) codes

  • Space and Planetary Science
  • Aerospace Engineering

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