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On regular reflection of detonation waves

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Abstract

The boundaries of regular reflection of detonation waves by a rigid wall are calculated. It is assumed that detonation is initiated at the point of reflection when a shock wave is incident on the wall at a finite angle in a gas fuel mixture, the detonation propagating instantaneously along the reflected front.

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Literature cited

  1. S. M. Gilinskii and G. G. Chernyi, “Supersonic flow of a fuel mixture past a sphere with allowance for the ignition delay time,” Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 1, 20 (1968).

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  2. G. G. Chernyi, “Self-similar problems of the flow of gas fuel mixtures past bodies,” Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 6, 10 (1966).

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Authors and Affiliations

  1. Frunze

    S. M. Urmambetov

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  1. S. M. Urmambetov
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Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 2, pp. 178–180, March–April, 1983.

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Urmambetov, S.M. On regular reflection of detonation waves. Fluid Dyn 18, 326–328 (1983). https://doi.org/10.1007/BF01091133

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  • DOI: https://doi.org/10.1007/BF01091133

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