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Calculation of supersonic flow past wings with consideration of tangential discontinuities shed from the edges within the scope of a model using a system of euler equations

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Literature cited

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  1. Moscow

    A. N. Minailos

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  1. A. N. Minailos
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Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 1, pp. 78–89, January–February, 1978.

The author thanks A. A. Dorodnitsyn, V. Ya. Neiland, and V. V. Sychev for useful discussions of the data.

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Minailos, A.N. Calculation of supersonic flow past wings with consideration of tangential discontinuities shed from the edges within the scope of a model using a system of euler equations. Fluid Dyn 13, 57–66 (1978). https://doi.org/10.1007/BF01094460

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  • DOI: https://doi.org/10.1007/BF01094460

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