Literature cited
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).
S. V. Fal'kovich, “On the theory of Laval nozzles,” Prikl. Matem. i Mekhan.,10, No. 4 (1946).
S. V. Fal'kovich, “Transonic plane gas flow with singularities on the sonic line,” Prikl. Matem. i Mekhan.,25, No. 2 (1961).
I. Biibosunov, “Example of plane-parallel transonic gas flow with a curve compression shock terminating within a flow with stream functions of the form ψ2/3=ρ2/2 f 2/3(θ/R),” Dokl. Akad. Nauk SSSR,126, No. 5 (1959).
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).
Author information
Authors and Affiliations
Additional information
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.
Rights and permissions
About this article
Cite this article
Biibosunov, I., Karybekov, N. Plane transonic flow by a curved compression shock. Fluid Dyn 5, 780–784 (1970). https://doi.org/10.1007/BF01017296
Received:
Issue Date:
DOI: https://doi.org/10.1007/BF01017296