Geodesic
Gas flowfield near the high altitude supersonic aircraft
Matematičeskoe modelirovanie, Tome 8 (1996) no. 6, pp. 13-18 Cet article a éte moissonné depuis la source Math-Net.Ru

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The work continues the investigation of the gas nowfield structure formed near the moving body with the dense reactive jet. The parameters of the jet and the outer flow are defined which provide the realisation of the inverse flow in the vicinity of the aircraft. 
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     author = {V. E. Gherm and E. V. Prozorova},
     title = {Gas flowfield near the high altitude supersonic aircraft},
     journal = {Matemati\v{c}eskoe modelirovanie},
     pages = {13--18},
     year = {1996},
     volume = {8},
     number = {6},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/MM_1996_8_6_a2/}
}
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V. E. Gherm; E. V. Prozorova. Gas flowfield near the high altitude supersonic aircraft. Matematičeskoe modelirovanie, Tome 8 (1996) no. 6, pp. 13-18. http://geodesic.mathdoc.fr/item/MM_1996_8_6_a2/