An investigation is made into the influence of the Mach number and the viscosity on the flow in the neighborhood of the trailing edge of a plate. The Mach number is assumed to satisfy m∞ 2 − 1 = 0(R−l/5), which corresponds to the regime of transonic interaction. It is shown that if the Mach number is such that ¦M∞ 2 − 1¦ > O(R−1/5) the problem in the region of free interaction can be reduced by an appropriate transformation to the already known solutions for an incompressible fluid  and supersonic flow .
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Translated from Izvestlya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 3, pp. 23–28, May–June, 1983.
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Korolev, G.L. Flow in the neighborhood of the trailing edge of a plate in a transonic flow of viscous gas. Fluid Dyn 18, 355–360 (1983). https://doi.org/10.1007/BF01090549
- Mach Number
- Incompressible Fluid
- Supersonic Flow
- Transonic Flow