Geodesic
The use of transonic slender-body theory to calculate the spatial flow over a wing–fuselage configuration
Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki, Tome 36 (1996) no. 9, pp. 134-154 Cet article a éte moissonné depuis la source Math-Net.Ru

Voir la notice de l'article

@article{ZVMMF_1996_36_9_a12,
     author = {V. V. Negoda and K. G. Sayadyan},
     title = {The use of transonic slender-body theory to calculate the spatial flow over a wing{\textendash}fuselage configuration},
     journal = {\v{Z}urnal vy\v{c}islitelʹnoj matematiki i matemati\v{c}eskoj fiziki},
     pages = {134--154},
     year = {1996},
     volume = {36},
     number = {9},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/ZVMMF_1996_36_9_a12/}
}
TY  - JOUR
AU  - V. V. Negoda
AU  - K. G. Sayadyan
TI  - The use of transonic slender-body theory to calculate the spatial flow over a wing–fuselage configuration
JO  - Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki
PY  - 1996
SP  - 134
EP  - 154
VL  - 36
IS  - 9
UR  - http://geodesic.mathdoc.fr/item/ZVMMF_1996_36_9_a12/
LA  - ru
ID  - ZVMMF_1996_36_9_a12
ER  - 
%0 Journal Article
%A V. V. Negoda
%A K. G. Sayadyan
%T The use of transonic slender-body theory to calculate the spatial flow over a wing–fuselage configuration
%J Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki
%D 1996
%P 134-154
%V 36
%N 9
%U http://geodesic.mathdoc.fr/item/ZVMMF_1996_36_9_a12/
%G ru
%F ZVMMF_1996_36_9_a12
V. V. Negoda; K. G. Sayadyan. The use of transonic slender-body theory to calculate the spatial flow over a wing–fuselage configuration. Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki, Tome 36 (1996) no. 9, pp. 134-154. http://geodesic.mathdoc.fr/item/ZVMMF_1996_36_9_a12/

[1] Malmuth N. D., Wu C. C., Cole J. D., Slender body theory and space shuttle transonic aerodynamics, AIAA Paper No 87-0478

[2] Fonarev A. S., Sayadyan K. G., Filatov O. G., “Metody rascheta aerodinamicheskikh kharakteristik elementov giperzvukovykh LA pri transzvukovykh skorostyakh poleta”, Aerotermodinamika vozdushno-kosmich. sistem, v. 1, TsAGI, M., 1992, 104–115

[3] Sayadyan K. G., Reshenie vnutrennei kraevoi zadachi transzvukovogo obtekaniya udlinennykh tel razlichnoi geometrii, Tr. TsAGI, 2487, M., 1990

[4] Rajagopal K., Malmuth N. D., Lick W. J., “Calculation of transonic flows over bodies of varying complexity using slender body theory”, AIAA Journal, 27:8 (1989), 1220–1229 | DOI

[5] Fu Qiang, “Calculation of transonic flow over bodies of varying complexity using similar perturbation method”, ICAS-92, 895–897

[6] Koul Dzh., Metody vozmuschenii v prikladnoi matematike, Mir, M., 1972 | MR

[7] Tretyakova I. V., Fonarev A. S., Transzvukovoe obtekanie tel vrascheniya s uchetom vliyaniya pronitsaemykh granits potoka, Tr. TsAGI, 2028, M., 1980

[8] Krupp J. A., Murman E. M., The numerical calculation of steady transonic flows past thin lifting airfoils and slender bodyes, AIAA Paper No 71-566

[9] Oswatitsch K., Keune F., “Ein Äquivalenzsatz für nicht angestrelte flugel kleiner Spanweite in schallnäher strömung”, Flügwissenschaft, 3:2 (1953), 29–46

[10] Koul Dzh., Kuk L., Transzvukovaya aerodinamika, Mir, M., 1989