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[1] Chakravarthy S. R., Szema K.-Y., “Euler solver for three-dimesional supersonic flows with subsonic pockets”, J. Aircraft, 24:2 (1987), 73–83 | DOI
[2] Lifshits Yu. B., Sakovich V. S., “O potentsialnom priblizhenii v teorii konicheskikh techenii”, Izv. AN SSSR. Mekhan. zhidkosti i gaza, 1990, no. 3, 112–118 | MR
[3] Siclari M. J., Supersonic nonlinear potential flows with subsonic regions and implicit isentropic shock fitting, AIAA Paper No 1201, 1981 | Zbl
[4] Shankar V., Szema K.-Y., Osher S., “A conservative type dependent full potential method for thetreatment of supersonic flows with embeded subsonic regions”, Proc. AIAA 6-th Comput. Fluid Dynamic Conf. (Danvers, Massachusetts, 1983), 36–47
[5] Lifshits Yu. B., Shagaev A. A., “Proektsionno-setochnaya skhema dlya rascheta obtekaniya profilya transzvukovym potokom”, Zh. vychisl. matem. i matem. fiz., 28:8 (1988), 1163–1176 | MR | Zbl
[6] Jameson A., “Transonic potential flow calculation using conservation form”, Proc. AIAA Second Comput. Fluid Dynamic Conf. (Hartford, Connecticut, 1975), 148–161
[7] Fedorenko P. P., “Relaksatsionnyi metod resheniya raznostnykh ellipticheskikh uravnenii”, Zh. vychisl. matem. i matem. fiz., 1:5 (1961), 922–927 | MR | Zbl
[8] South J. C., Keller J. D., Hafez M. M., “Vector processor algorithms for transonic flow calculations”, AIAA Journal, 18:7 (1980), 786–792 | DOI
[9] Butler D. S., “The numerical solution of hyperbolic systems of partial differential equation in three independent variables”, Proc. Roy. Soc. London A, 255 (1960), 232–250 | DOI | MR
[10] M. Khemsh, Dzh. Nilsen, Aerodinamika raket, v. 2, Mir, M., 1989, 255–295