Abstract
The results of theoretical investigation of an ideal-gas asymmetrical flow around V-shaped wings with an opening angle exceeding π and having supersonic forward edges at all modes are presented.
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M. A. Zubin, F. A. Maksimov, and N. A. Ostapenko, Fluid Dyn., No. 6, 804 (2014).
A. L. Gonor and N. A. Ostapenko, Izv. Akad. Nauk SSSR, No. 3, 46 (1970).
M. A. Zubin and N. A. Ostapenko, Izv. Akad. Nauk SSSR, No. 4, 130 (1975).
F. A. Maksimov and N. A. Ostapenko, Proc. X-th Intern. Conf. on Nonequil. Proc. in Nozzles and Jets (Izd-vo MAI, Moscow, 2014) [in Russian].
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Original Russian Text © F.A. Maksimov, N.A. Ostapenko, 2016, published in Doklady Akademii Nauk, 2016, Vol. 469, No. 6, pp. 680–685.
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Maksimov, F.A., Ostapenko, N.A. V-shaped wings with an opening angle exceeding π at super- and hypersonic flow velocities. Dokl. Phys. 61, 412–417 (2016). https://doi.org/10.1134/S1028335816080139
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DOI: https://doi.org/10.1134/S1028335816080139