An efficient method for calculating the spatial flow around air intakes at transonic speeds
Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki, Tome 31 (1991) no. 9, pp. 1355-1368 Cet article a éte moissonné depuis la source Math-Net.Ru

Voir la notice de l'article

@article{ZVMMF_1991_31_9_a8,
     author = {D. A. Lyubimov},
     title = {An efficient method for calculating the spatial flow around air intakes at transonic speeds},
     journal = {\v{Z}urnal vy\v{c}islitelʹnoj matematiki i matemati\v{c}eskoj fiziki},
     pages = {1355--1368},
     year = {1991},
     volume = {31},
     number = {9},
     language = {ru},
     url = {http://geodesic.mathdoc.fr/item/ZVMMF_1991_31_9_a8/}
}
TY  - JOUR
AU  - D. A. Lyubimov
TI  - An efficient method for calculating the spatial flow around air intakes at transonic speeds
JO  - Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki
PY  - 1991
SP  - 1355
EP  - 1368
VL  - 31
IS  - 9
UR  - http://geodesic.mathdoc.fr/item/ZVMMF_1991_31_9_a8/
LA  - ru
ID  - ZVMMF_1991_31_9_a8
ER  - 
%0 Journal Article
%A D. A. Lyubimov
%T An efficient method for calculating the spatial flow around air intakes at transonic speeds
%J Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki
%D 1991
%P 1355-1368
%V 31
%N 9
%U http://geodesic.mathdoc.fr/item/ZVMMF_1991_31_9_a8/
%G ru
%F ZVMMF_1991_31_9_a8
D. A. Lyubimov. An efficient method for calculating the spatial flow around air intakes at transonic speeds. Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki, Tome 31 (1991) no. 9, pp. 1355-1368. http://geodesic.mathdoc.fr/item/ZVMMF_1991_31_9_a8/

[1] Holst T. L., “Fast, conservative algorithm for solving the transonic full-potential equation”, AIAA J., 18:12 (1980), 1431–1439 | DOI | Zbl

[2] Atta E. H., Vadyak J., Three-dimentional transonic naccele/inlet flowfield computations using an efficient approximate factorization algorithm, AIAA paper, No 83-1417, 1983

[3] Peace A. J., Transonic flow calculations around isolated inlet configurations, AIAA paper, No 85-1596, 1985

[4] Takashi N., “Computation of three-dimentional transonic inlet flowfields using an approximate factorization algorithm”, J. Propulsion, 4:3 (1988), 285–287 | DOI

[5] Ivanov M. Ya., Koretskii V. V., “Raschet techenii v dvumernykh i prostranstvennykh soplakh metodom priblizhennoi faktorizatsii”, Zh. vychisl. matem. i matem. fiz., 25:9 (1985), 1365–1381 | MR

[6] Koretskii V. V., Lyubimov D. A., “Modifitsirovannyi metod priblizhennoi faktorizatsii dlya rascheta potentsialnykh prostranstvennykh techenii v kanalakh”, Zh. vychisl. matem. i matem. fiz., 30:10 (1990), 1553–1570 | MR

[7] Flores J., Holst T. L., Kwak D., Batiste D., “A new consistent spatial differencing scheme for the transonic potential equation”, AIAA J., 22:8 (1984), 1027–1034 | DOI | MR | Zbl

[8] Jiang H., Cai R., An accurate spatial differencing scheme with suitability to curvilinear grids for 3-D full-potential flow computation, AIAA paper, No 85-1662, 1985

[9] South J. C., Hafez M. M., Stability analysis of intermediate boundary conditions in approximate factorization schemes, AIAA paper, No 83-1898, 1983 | Zbl

[10] Catherall D., “Optimum approximate factorization schemes for two-dimensional steady potential flows”, AIAA J., 20:3 (1982), 1057–1063 | DOI | MR | Zbl

[11] Catherall D., “The optimization of aproximate factorization schemes for solving elliptic partial differential equations in three dimensions, featuring a new two-factor scheme”, J. Comput. Phys., 78:2 (1988), 138–159 | DOI | MR | Zbl

[12] Forester C. K., Body-fitted 3-D full potential flow analysis of complex ducts and inlets, AIAA paper, No 81-2, 1981

[13] Miller B. A., Dastoli B. J., Wesoky H. L., Effect of entry-lip design on aerodynamics and acoustics of high throat Mach number inlet for the quiet, clean, shorthoul experimental engine, NASA TM, No X-3222, 1975

[14] Burley R. R., Effect of lip center body geometry on aerodynamic of inlet for tilting-naccelle VTOL aircraft, AIAA paper,No 79-381, 1979