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中文核心期刊
MACH NUMBER EFFECTS ON SEPARATION BEHAVIORS INDUCED BY SWEPT SHOCK WAVE[J]. Chinese Journal of Theoretical and Applied Mechanics, 1995, 27(S): 98-102. DOI: 10.6052/0459-1879-1995-S-1995-509
Citation: MACH NUMBER EFFECTS ON SEPARATION BEHAVIORS INDUCED BY SWEPT SHOCK WAVE[J]. Chinese Journal of Theoretical and Applied Mechanics, 1995, 27(S): 98-102. DOI: 10.6052/0459-1879-1995-S-1995-509

MACH NUMBER EFFECTS ON SEPARATION BEHAVIORS INDUCED BY SWEPT SHOCK WAVE

  • An experimental investigation was made for the shock wave/turbulent boundary-layer interactions induced by swept compression corners.The techniques used in this studywere the surface pressure distribution measurement and surface oil-film streak visualization.Effects of upstream Mach number M_∞ on the behavior of separation and the condition forincipient separation were mainly studied. The test Mach numbers were 1.79,2.04 and 2.50and the Reynolds numbers were about 2.42 2.47×10 ̄7/m。 15 compression corner mo...
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