Geodesic
Calculation of the performance characteristics of a three-dimensional scramjet nozzle/afterbody system
Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki, Tome 38 (1998) no. 2, pp. 337-343 Cet article a éte moissonné depuis la source Math-Net.Ru

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     author = {M. K. Aukin and R. K. Tagirov},
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M. K. Aukin; R. K. Tagirov. Calculation of the performance characteristics of a three-dimensional scramjet nozzle/afterbody system. Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki, Tome 38 (1998) no. 2, pp. 337-343. http://geodesic.mathdoc.fr/item/ZVMMF_1998_38_2_a16/

[1] Aukin M. K., Tagirov R. K., “Konechno-raznostnaya skhema vtorogo poryadka dlya rascheta trekhmernykh sverkhzvukovykh techenii idealnogo gaza”, Zh. vychisl. matem. i matem. fiz., 29:7 (1989), 1057–1066 | MR | Zbl

[2] Ishiguro T., Takaki R. T., Mitani T., Hiraiwa T., Three-dimensional analysis of scramjet nozzle flows, AIAA paper No 5059, 1993