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

[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