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Penetration of a jet blown through a convex cylindrical surface into a supersonic stream

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Literature cited

  1. V. F. Zakharchenko and Yu. Kh. Kardanov, “Geometry of a liquid wing in a supersonic flow,” Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 2, 157 (1980).

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  2. J. A. Schetz, “Shape of the shock wave when a transverse jet interacts with a supersonic flow,” Aviastroenie, Ekspress-Inform., No. 45, 21 (1970).

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  3. V. S. Avduevskii, K. I. Medvedev, and M. N. Polyanskii, “Interaction of a supersonic flow with a transverse jet blown through a circular opening in a plate,” Izv. Akad. Nauk SSSR, Mekh. Zhidk. Gaza, No. 5, 193 (1970).

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Authors and Affiliations

  1. Moscow

    V. F. Zakharchenko, Yu. Kh. Kardanov & A. N. Semenikhin

Authors
  1. V. F. Zakharchenko
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  2. Yu. Kh. Kardanov
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  3. A. N. Semenikhin
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Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 1, pp. 187–190, January–February, 1983.

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Zakharchenko, V.F., Kardanov, Y.K. & Semenikhin, A.N. Penetration of a jet blown through a convex cylindrical surface into a supersonic stream. Fluid Dyn 18, 161–164 (1983). https://doi.org/10.1007/BF01090529

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  • DOI: https://doi.org/10.1007/BF01090529

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