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Plane transonic flow by a curved compression shock

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Literature cited

  1. I. Biibosunov and N. Karybekov, “Solution of the Chaplygin equation in plane-parallel transonic flow with a normal compression shock,” Izv. Akad. Nauk SSSR, Mekhan. Zhidk. i Gaza, No. 2 (1967).

  2. S. V. Fal'kovich, “On the theory of Laval nozzles,” Prikl. Matem. i Mekhan.,10, No. 4 (1946).

  3. S. V. Fal'kovich, “Transonic plane gas flow with singularities on the sonic line,” Prikl. Matem. i Mekhan.,25, No. 2 (1961).

  4. I. Biibosunov, “Example of plane-parallel transonic gas flow with a curve compression shock terminating within a flow with stream functions of the form ψ2/32/2 f 2/3(θ/R),” Dokl. Akad. Nauk SSSR,126, No. 5 (1959).

  5. F. I. Frankl', “Subsonic flow around a profile with a local supersonic zone terminating in a curved compression shock,” Prikl. Matem. i Mekhan.,21, No. 1 (1957).

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Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 5, pp. 78–83, September–October, 1970.

The authors are grateful to S. V. Fal'kovich for discussing the results of the research.

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Biibosunov, I., Karybekov, N. Plane transonic flow by a curved compression shock. Fluid Dyn 5, 780–784 (1970). https://doi.org/10.1007/BF01017296

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  • DOI: https://doi.org/10.1007/BF01017296

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