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Separated flows induced by the interaction between the shock wave ahead of a conic internal-compression obstacle and the boundary layer

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Abstract

Specific features of three-dimensional separated flows induced by the interaction between a conic convergent shock and the boundary layer are experimentally studied for supersonic flow velocities. The data demonstrate the formation of separated-flow zones whose properties were not registered in earlier studies.

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Authors
  1. A. I. Glagolev
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  2. A. I. Zubkov
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  3. K. A. Taabaldiev
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Additional information

Moscow. Translated from Izvestiya Rossiiskoi Akademii Nauk, Mekhanika Zhidkosti i Gaza, No. 1, pp. 147–151, January–February, 1995.

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Glagolev, A.I., Zubkov, A.I. & Taabaldiev, K.A. Separated flows induced by the interaction between the shock wave ahead of a conic internal-compression obstacle and the boundary layer. Fluid Dyn 30, 120–123 (1995). https://doi.org/10.1007/BF02029936

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  • DOI: https://doi.org/10.1007/BF02029936

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