On a solution of an iverse problem for internal vicous flows with a supersonic kernel
Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki, Tome 31 (1991) no. 5, pp. 790-793 Cet article a éte moissonné depuis la source Math-Net.Ru

Voir la notice de l'article

@article{ZVMMF_1991_31_5_a15,
     author = {S. G. Karataev and V. N. Koterov},
     title = {On a~solution of an iverse problem for internal vicous flows with a~supersonic kernel},
     journal = {\v{Z}urnal vy\v{c}islitelʹnoj matematiki i matemati\v{c}eskoj fiziki},
     pages = {790--793},
     year = {1991},
     volume = {31},
     number = {5},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/ZVMMF_1991_31_5_a15/}
}
TY  - JOUR
AU  - S. G. Karataev
AU  - V. N. Koterov
TI  - On a solution of an iverse problem for internal vicous flows with a supersonic kernel
JO  - Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki
PY  - 1991
SP  - 790
EP  - 793
VL  - 31
IS  - 5
UR  - http://geodesic.mathdoc.fr/item/ZVMMF_1991_31_5_a15/
LA  - ru
ID  - ZVMMF_1991_31_5_a15
ER  - 
%0 Journal Article
%A S. G. Karataev
%A V. N. Koterov
%T On a solution of an iverse problem for internal vicous flows with a supersonic kernel
%J Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki
%D 1991
%P 790-793
%V 31
%N 5
%U http://geodesic.mathdoc.fr/item/ZVMMF_1991_31_5_a15/
%G ru
%F ZVMMF_1991_31_5_a15
S. G. Karataev; V. N. Koterov. On a solution of an iverse problem for internal vicous flows with a supersonic kernel. Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki, Tome 31 (1991) no. 5, pp. 790-793. http://geodesic.mathdoc.fr/item/ZVMMF_1991_31_5_a15/

[1] Pirumov U. G., “Raschet techeniya v sople Lavalya”, Izv. AN SSSR. Mekhan. zhidkosti i gaza, 1967, no. 5, 10–22

[2] Cohen M. J., Portnoy H., “Irrotational subsonic flow of an ideal gas in two-dimensional ducts — optimal ducts and ducts with plane sonic exits”, AIAA Journal, 12:5 (1974), 608–614 | DOI

[3] Ovsyannikov A. M., “Raschet techeniya v dozvukovoi i transzvukovoi chastyakh koltsevykh sopel”, Izv. AN SSSR. Mekhan. zhidkosti i gaza, 1971, no. 6, 137–143

[4] Osipov I. A., Shipilin A. V., Shulishnina N. P., “O forme dozvukovoi chasti sopla s ploskoi dozvukovoi poverkhnostyu pri uchete vyazkosti v priblizhenii pogranichnogo sloya”, Inzh.-fiz. zh., 42:5 (1982), 724–729

[5] Koterov V. N., Osipov I. L., Paschenko V. P., “O profilirovanii ploskogo sverkhzvukovogo sopla, obespechivayuschego ravnomernyi potok v vykhodnom sechenii”, Uch. zap. TsAGI, 18:3 (1987), 48–56

[6] Lin T. C., Rubin S. G., A numerical model for supersonic viscous flow over a slender reentry vehicle, AIAA Paper No 205, 1979, 10 pp.

[7] Voinovich P. A., Fursenko A. A., Raschet struinykh i vnutrennikh techenii vyazkogo gaza, Preprint No 860, LFTI AN SSSR, L., 1983, 23 pp.

[8] Karataev S. G., Koterov V. N., “Chislennyi metod rascheta sverkhzvukovykh techenii vyazkogo gaza”, Zh. vychisl. matem. i matem. fiz., 30:4 (1990), 586–600 | MR | Zbl

[9] Pchelkina A. V., Solodkin V. K., “Korrektirovka vliyaniya pogranichnogo sloya na techenie v sople s izlomom obrazuyuschei”, Chisl. metody v gazovoi dinamike, Izd-vo MGU, M., 1965, 103–107

[10] Sivells J. C., “Aerodynamic design of axisymmetric wind-tunnel nozzly”, J. Space and Rockets, 7:11 (1970), 35–43