@article{ZVMMF_1992_32_4_a8,
author = {P. M. Byval'tsev},
title = {A method of calculating the flow around and aerodynamic design of the profiles of turbomachinery blade grids},
journal = {\v{Z}urnal vy\v{c}islitelʹnoj matematiki i matemati\v{c}eskoj fiziki},
pages = {598--612},
year = {1992},
volume = {32},
number = {4},
language = {ru},
url = {http://geodesic.mathdoc.fr/item/ZVMMF_1992_32_4_a8/}
}
TY - JOUR AU - P. M. Byval'tsev TI - A method of calculating the flow around and aerodynamic design of the profiles of turbomachinery blade grids JO - Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki PY - 1992 SP - 598 EP - 612 VL - 32 IS - 4 UR - http://geodesic.mathdoc.fr/item/ZVMMF_1992_32_4_a8/ LA - ru ID - ZVMMF_1992_32_4_a8 ER -
%0 Journal Article %A P. M. Byval'tsev %T A method of calculating the flow around and aerodynamic design of the profiles of turbomachinery blade grids %J Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki %D 1992 %P 598-612 %V 32 %N 4 %U http://geodesic.mathdoc.fr/item/ZVMMF_1992_32_4_a8/ %G ru %F ZVMMF_1992_32_4_a8
P. M. Byval'tsev. A method of calculating the flow around and aerodynamic design of the profiles of turbomachinery blade grids. Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki, Tome 32 (1992) no. 4, pp. 598-612. http://geodesic.mathdoc.fr/item/ZVMMF_1992_32_4_a8/
[1] Hicks R. M., Henne P. A., Wing design by numerical optimization, AIAA Paper No 77-1247, 1977 pp.
[2] Davis W. M., Technique for developing design tools from the analysis methods of computational aerodynamics, AIAA Paper No 79-1529, 1979 pp.
[3] Garabedian P., McFadden G., “Design of supercritical swept wings”, AIAA Journal, 20:3 (1982), 289–291 | DOI | MR | Zbl
[4] Tranen T. L., A rapid computer aided transonic airfoil design method, AIAA Paper No 74-501, 1974
[5] Cedar R. D., Stow P., “A compatible mixed design and analysis finite element method for the design of turbomachinery blades”, Internat. J. Numer. Methods in Fluids, 5 (1985), 331–345 | DOI | Zbl
[6] Hart M., Whitehead D. S., “A design method for two-dimensional cascades of turbomachinery blades”, Internat. J. Numer. Methods in Fluids, 7 (1987), 1363–1381 | DOI | Zbl
[7] Dulikravich D. S., Sobetskii Kh., “Reshenie zadachi transzvukovogo obtekaniya reshetki profilei i modifikatsiya formy profilei dlya ustraneniya udarnykh voln v mezhlopatochnykh kanalakh”, Aerokosmich. tekhn., 1:6 (1983), 70–78
[8] Bauer F., Garabedian P., Korn D., “Supercritical wing sections, III”, Lect. Notes in Economics and Math. Systems, Springer, N. Y., 1975, 150
[9] Lighthile M. J., A mathematical method of cascade design, British Aeronaut. Res. Council. R M 2104, 1945
[10] Stanitz J. D., Design of two-dimensional channels walls, NACA Rept. No 1115, 1953 | MR
[11] Ackeret J., The design of closely spaced blade grids, British M. A. P. R. T. P. Trans. 2007, 1942
[12] Strand T., “Exact method of designing airfoils with given velocity distribution incompressible flow”, J. Aircraft, 10:11 (1975), 651–659 | DOI
[13] Volp G., Melnik P. E., “Metod proektirovaniya zamknutykh profilei s proizvolnym sverkhkriticheskim raspredeleniem skorostei”, Aerokosmich. tekhn., 1987, no. 4, 66–76
[14] Elizarov A. M., Ilinskii N. B., Potashev A. V., “Postroenie krylovykh profilei metodom kvazireshenii obratnykh kraevykh zadach”, Izv. AN SSSR. Mekhan. zhidkosti i gaza, 1988, no. 3, 5–13 | MR | Zbl
[15] Tumashev G. G., “Opredelenie formy granits potoka zhidkosti po zadannomu raspredeleniyu skorosti ili davleniya”, Uch. zap. Kazanskogo un-ta, 112, no. 3, 1952, 3–41
[16] Stepanov G. Yu., Gidrodinamika reshetok turbomashin, Fizmatgiz, M., 1962
[17] Dzhailz M. B., Drila M., “Metod proektirovaniya transzvukovykh profilei”, Aerokosmich. tekhn., 1988, no. 6, 13–22
[18] Osipov I. L., Shipilin A. V., Shulishnina N. P., “Chislennyi metod rascheta techenii gazov v kanalakh i soplakh v pryamoi, obratnoi i kombinirovannoi postanovkakh”, Zh. vychisl. matem. i matem. fiz., 27:10 (1987), 1563–1572 | Zbl
[19] Gostelou Dzh., Aerodinamika reshetok turbomashin, Mir, M., 1987
[20] Aksentev L. A., Ilinskii N. B., Nutin M. T. i dr., “Teoriya obratnykh kraevykh zadach dlya analiticheskikh funktsii i ee prilozheniya”, Itogi nauki i tekhn. Matem. analiz, 18, VINITI, M., 1980, 67–124 | MR
[21] Stone H. L., “Iterative solution of implicit approximations of multi-dimensional partial differential equations”, SIAM J. Numer. Analys., 5:3 (1968), 530–558 | DOI | MR | Zbl
[22] Byvaltsev P. M., Ivanov M. Ya., “Metod rascheta potentsialnykh transzvukovykh techenii v reshetkakh turbomashin”, Zh. vychisl. matem. i matem. fiz., 29:3 (1989), 447–459 | MR
[23] 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
[24] Flores J., Holst T. L., Kwak D., Batiste D. M., “A new consistent spatial differencing scheme for the transonic full-potential equation”, AIAA Journal, 22:8 (1984), 1027–1034 | DOI | MR | Zbl
[25] Lifshits Yu. B., Shagaev A. A., “O potentsialnykh modelyakh transzvukovykh techenii”, Dokl. AN SSSR, 304:6 (1989), 1315–1319 | Zbl
[26] Malone J. B., Sankar N. L., “Numerical simulation of two-dimensional unsteady transonic flow using the full-potential equation”, AIAA Journal, 22:8 (1984), 1035–1041 | DOI | Zbl
[27] Sankar N. L., Malone J. B., Tassa Y., “A strongly implicit procedure for steady three-dimensional transonic potential flows”, AIAA Journal, 20:5 (1982), 598–605 | DOI | Zbl
[28] Nili D. A., Mikhelk M. S., Khilton L. D., Gledden X. Dzh., “Izmereniya raspredeleniya teplootdachi na poverkhnostyakh vysokonagruzhennykh lopatok soplovogo apparata turbiny”, Energetich. mashiny, 106:1 (1984), 86–96