Abstract
The limiting flow parameters are determined directly behind the central shock for Mach numbers M ≫ 1 in front of the shock. A formula for the Mach number distribution over the jet axis is derived.
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Subscripts denote the gas parameters.
Translated from Inzhenerno-Fizicheskii Zhurnal, Vol. 15, No. 6, pp. 982–987, December, 1968.
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Finat'ev, Y.P., Shcherbakov, L.A. & Gorskaya, N.M. Mach number distribution over the axis of supersonic underexpanded jets. Journal of Engineering Physics 15, 1153–1157 (1968). https://doi.org/10.1007/BF00828936
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DOI: https://doi.org/10.1007/BF00828936