Abstract
The paper presents exact particular solutions of the equations of transonic gas flows, analogous to the solutions derived in [1–3] for the case of short waves. These solutions are used to construct the flow around a body in a supersonic stream with an attached shock.
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References
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O. S. Ryzhov and G. M. Shefter, “On nonsteady gas flows in Laval nozzles,” AN SSSR, vol. 128, no. 3, 1959.
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Zaslavskii, B.I., Klepikova, N.A. On a class of exact particular solutions of the equations of transonic gas flows. J Appl Mech Tech Phys 6, 42–44 (1965). https://doi.org/10.1007/BF00919310
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DOI: https://doi.org/10.1007/BF00919310