Abstract
The effect of the expansion rate n on the withdrawal Δ of the shock and the relative pressure at the stagnation point is studied for a jet flowing onto an infinite plane barrier placed perpendicular to the jet axis.
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Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 32, No. 2, pp. 247–250, February, 1977.
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Sokolov, E.I., Startsev, A.V., Uskov, V.N. et al. Limiting expansion ratio of a supersonic jet flowing onto a perpendicular infinite plane barrier. Journal of Engineering Physics 32, 149–152 (1977). https://doi.org/10.1007/BF00858500
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DOI: https://doi.org/10.1007/BF00858500