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The reflection of a plane shock wave from a body with groove

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Abstract

When a plane shock wave impinges on bodies with grooves and when a supersonic stream of gas flows past such bodies a complicated flow pattern develops. In a number of cases oscillations of the bow wave [1–3] and an anomalous heating of the gas in the groove [4–6] have been observed. Unsteady reflection of shock waves from bodies with grooves and the processes occurring inside the grooves have been investigated comparatively little.

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Literature cited

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Authors and Affiliations

  1. Moscow

    M. A. Ibragim, A. O. Serov, L. S. Shtemenko & F. V. Shugaev

Authors
  1. M. A. Ibragim
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  2. A. O. Serov
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  3. L. S. Shtemenko
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  4. F. V. Shugaev
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Additional information

Translated from Izvestiya Akademii Nauk SSSR, Hekhanika Zhidkosti 1 Gaza, No. 5, pp. 180–186, September–October, 1935.

The authors wish to thank V. I. Ivanov for carrying out the calculations.

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Ibragim, M.A., Serov, A.O., Shtemenko, L.S. et al. The reflection of a plane shock wave from a body with groove. Fluid Dyn 20, 822–828 (1985). https://doi.org/10.1007/BF01050102

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  • DOI: https://doi.org/10.1007/BF01050102

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