Abstract
The method of integral relations [1] and the method of characteristics are used to construct a scheme for the numerical solution of the problem of the interaction of a supersonic underexpanded jet with an obstacle. The results of calculations are presented.
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References
O. M. Belotserkovskii, “On the calculation of flow about axisymmetric bodies with detached shock on an electronic computer”, PMM, vol. 24, no. 3, 1960.
N. E. Khramov, “Calculation of nonuniform gas flow past a sphere”, PMM, vol. 29, no. 1, 1965.
F. E. Ehlers, “Method of characteristics for isoenergetic supersonic flows, adapted for high speed digital computers”, collection: Mechanics [collection of translations and summaries of foreign periodicals], 1(59), 1960.
O. N. Katskova, I. N. Naumova, Yu. D. Shmyglevskii, and N. P. Shulishnina, “Experience in calculating two-dimensional and axisymmetric supersonic gas flows by the method of characteristics”, VTs AN SSSR, 1961.
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The author wishes to thank his scientific coworker I. I. Kuhlin for compiling and debugging the program.
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Khramov, N.E. Calculation of the interaction of an axisymmetric supersonic underexpanded jet with an obstacle. Fluid Dyn 1, 90–93 (1966). https://doi.org/10.1007/BF01022162
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DOI: https://doi.org/10.1007/BF01022162