Abstract
Numerical simulation of the flow of a supersonic stream of viscous, compressible, heat-conducting gas over a cavity is carried out on the basis of kinetically consistent difference schemes. Different types of flow (“open” and “closed” cavities) are considered, the heat fluxes to the walls of the recess are determined, and a nonsteady regime of flow over a cavity is simulated. The results obtained are compared with known experimental relationships.
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Translated from Inzhenerno-fizicheskii Zhurnal, Vol. 61, No. 4, pp. 570–577, October, 1991.
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Graur, I.A., Elizarova, T.G. & Chetverushkin, B.N. Numerical simulation of the flow of a supersonic stream of viscous compressible gas over a cavity. Journal of Engineering Physics 61, 1212–1218 (1991). https://doi.org/10.1007/BF00872588
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DOI: https://doi.org/10.1007/BF00872588