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Asymmetric interaction of blast waves and shock waves with a body flying at supersonic velocity

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Abstract

The problems of asymmetric interaction of a blunt wedge traveling at supersonic velocity with a cylindrical blast wave from a point explosion and with a plane shock wave are investigated by numerical simulation. The evolution of the interaction flow is analyzed, and data are obtained on how the structure of the shock layer changes.

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Authors and Affiliations

  1. A. F. Ioffe Physicotechnical Institute, Russian Academy of Sciences, 194021, St. Petersburg, Russia

    V. P. Goloviznin & I. V. Krasovskaya

Authors
  1. V. P. Goloviznin
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  2. I. V. Krasovskaya
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Zh. Tekh. Fiz. 69, 15–19 (May 1999)

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Goloviznin, V.P., Krasovskaya, I.V. Asymmetric interaction of blast waves and shock waves with a body flying at supersonic velocity. Tech. Phys. 44, 493–496 (1999). https://doi.org/10.1134/1.1259371

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  • DOI: https://doi.org/10.1134/1.1259371

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