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Effect of a weak shock on a wing of complex planform at supersonic speeds

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Literature cited

  1. A. I. Golubinskii, “On the flow around a moving plate by a shifting shock,” Inzh. Zh.,1, No. 2 (1961).

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Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 2, pp. 173–176, March–April, 1974.

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Shamshurin, A.D. Effect of a weak shock on a wing of complex planform at supersonic speeds. Fluid Dyn 9, 311–314 (1974). https://doi.org/10.1007/BF01092671

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  • DOI: https://doi.org/10.1007/BF01092671

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