Literature cited
A. I. Golubinskii, “On the flow around a moving plate by a shifting shock,” Inzh. Zh.,1, No. 2 (1961).
E. A. Krasil'shchikova, “Finite span wing in the presence of a moving shock,” Izv. Akad. Nauk SSSR, Mekhan. Mashinostr., No. 5 (1964).
E. A. Krasil'shchikova, “Thin wing in the presence of a moving pressure wave of finite extent,” Izv. Akad. Nauk SSSR, Mekhan. Zhidk. Gaza, No. 1 (1966).
E. F. Ehlers and E. M. Shoemaker, “A linearized analysis of the forces exerted on a rigid wing by a shock wave,” J. Aerospace Sci.,26, No. 2 (1959).
S. M. Belotserkovskii and S. A. Popytalov, “Analysis of the effect of a gust on a wing with subsonic leading and trailing edges,” Izv. Akad. Nauk SSSR, Mekhan. Zhidk. Gaza, No. 12 (1970).
S. M. Belotserkovskii, B. K. Skripach, and V. G. Tabachnikov, Wing in a Nonstationary Gas Flow [in Russian], Nauka, Moscow (1971).
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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