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Investigation of the interaction between a supersonic jet and a subsonic cocurrent-flow and an obstacle

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Literature cited

  1. V. V. Eremin and Yu. M. Lipnitskii, “Difference scheme of third-order accuracy for computation of two-dimensional flows with a contact discontinuity,” Scientific Work of the Moscow State Uaiversity Institute of Mechanics, No. 19 (1972).

  2. L. D. Landau and E. M. Lifshits, Fluid Mechanics, Addison-Wesley (1959).

  3. R. Mises, Mathematical Theory of Compressible Fluid Flow, Academic (1958).

  4. K. G. Guderley, Theory of Transonic Flow, Addison-Wesley (1962).

  5. A. A. Nikol'skii and G. I. Taganov, “Gas motion in a local supersonic zone aad some conditions of spoiling potential flow,” Prikl. Matem. Mekhan.,10, No. 4 (1946).

  6. É. G. Shifrin, “On the problem of a supersonic jet flowing around an infinite wedge,” Izv. Akad. Nauk SSSR, Mekhan. Zhidk. Gaza, No. 2 (1969).

  7. É. G. Shifrin, “On the problem of a uniform supersonic jet flowing around a profile,” Izv. Akad. Nauk SSSR, Mekhan. Zhidk. Gaza, No. 4 (1972).

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Authors and Affiliations

  1. Moscow

    V. V. Eremin, Yu. M. Lipnitskii & É. G. Shifrin

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  1. V. V. Eremin
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  2. Yu. M. Lipnitskii
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  3. É. G. Shifrin
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Additional information

Translated from Izvestiya Akademiya Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 3, pp. 170–173, May–June, 1974.

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Eremin, V.V., Lipnitskii, Y.M. & Shifrin, É.G. Investigation of the interaction between a supersonic jet and a subsonic cocurrent-flow and an obstacle. Fluid Dyn 9, 482–485 (1974). https://doi.org/10.1007/BF01025539

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  • DOI: https://doi.org/10.1007/BF01025539

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