Fluid Dynamics

, Volume 5, Issue 4, pp 609–613 | Cite as

Plane-parallel supersonic flow with a discontinuity

  • I. Biibosunov
  • A. Ryskulov
Article

Abstract

This article considers a plant-parallel supersonic flow, with a shock wave terminating within the flow; the shock wave is regarded as a distortion. A line of discontinuity is located ahead of the shock wave in the supersonic zone. The problem is solved by the method of indeterminate coefficients.

Keywords

Shock Wave Supersonic Flow Supersonic Zone Indeterminate Coefficient 

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Literature cited

  1. 1.
    F. I. Frankl', “An example of a supersonic flow of gas, with a region of supersonic velocities bounded downstream by a shock wave terminating within the flow,” Prikl. Mat. i Mekh.,19 No. 4 (1955).Google Scholar
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    I. B. Biibosunov, “An example of a supersonic flow of gas, with a region of supersonic velocities bounded downstream by a distorted shock wave terminating within the flow,” Prikl. Mat. i Mekh.,22 No. 3 (1958).Google Scholar
  3. 3.
    I. B. Biibosunov, “Refinement of one example of supersonic flow,” Inzh. Zh.,3, No. 3 (1963).Google Scholar
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    S. V. Fal'kovich, “The theory of a Laval nozzle,” Pril. Mat. i Mekh.,10, No. 4 (1946).Google Scholar
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    F. I. Frankl', “The flow profile of a subsonic flow, with a local supersonic zone terminating in a distorted shock wave,” Prikl. Mat. i Mekh.,21, No. 1 (1957).Google Scholar

Copyright information

© Consultants Bureau 1973

Authors and Affiliations

  • I. Biibosunov
    • 1
  • A. Ryskulov
    • 1
  1. 1.Frunze

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