Geodesic
Gas flowfield near the high altitude supersonic aircraft
Matematičeskoe modelirovanie, Tome 8 (1996) no. 6, pp. 13-18.

Voir la notice de l'article provenant de la source Math-Net.Ru

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. 
@article{MM_1996_8_6_a2,
     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},
     publisher = {mathdoc},
     volume = {8},
     number = {6},
     year = {1996},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/MM_1996_8_6_a2/}
}
TY  - JOUR
AU  - V. E. Gherm
AU  - E. V. Prozorova
TI  - Gas flowfield near the high altitude supersonic aircraft
JO  - Matematičeskoe modelirovanie
PY  - 1996
SP  - 13
EP  - 18
VL  - 8
IS  - 6
PB  - mathdoc
UR  - http://geodesic.mathdoc.fr/item/MM_1996_8_6_a2/
LA  - ru
ID  - MM_1996_8_6_a2
ER  - 
%0 Journal Article
%A V. E. Gherm
%A E. V. Prozorova
%T Gas flowfield near the high altitude supersonic aircraft
%J Matematičeskoe modelirovanie
%D 1996
%P 13-18
%V 8
%N 6
%I mathdoc
%U http://geodesic.mathdoc.fr/item/MM_1996_8_6_a2/
%G ru
%F MM_1996_8_6_a2
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/