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Effects of Mach number on turbulent separation behaviours induced by blunt fin

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Abstract

 An experimental study of the interaction between shock wave and turbulent boundary layer induced by blunt fin has been carried out at M ∞=7.8 using oil flow visualization and simultaneous measurements of fluctuating wall pressure and heat transfer. This paper presents the effects of Mach number on turbulent separation behaviours induced by blunt fin.

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Authors and Affiliations

  1. Laboratory of High Temperature Dynamics Institute of Mechanics, Chinese Academy of Sciences Beijing 100080, P.R. China, , , , , , CN

    S. F. Wang, Z. Y. Ren & Y. Wang

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  1. S. F. Wang
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  2. Z. Y. Ren
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  3. Y. Wang
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Received: 21 July 1996/Accepted: 4 February 1998

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Wang, S., Ren, Z. & Wang, Y. Effects of Mach number on turbulent separation behaviours induced by blunt fin. Experiments in Fluids 25, 347–351 (1998). https://doi.org/10.1007/s003480050239

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  • DOI: https://doi.org/10.1007/s003480050239

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