Geodesic
A conformally integral method for solving a direct problem of aerodynamics of turbomachine blade rows
Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki, Tome 32 (1992) no. 7, pp. 1145-1148 Cet article a éte moissonné depuis la source Math-Net.Ru

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F. F. Nevzorov. A conformally integral method for solving a direct problem of aerodynamics of turbomachine blade rows. Žurnal vyčislitelʹnoj matematiki i matematičeskoj fiziki, Tome 32 (1992) no. 7, pp. 1145-1148. http://geodesic.mathdoc.fr/item/ZVMMF_1992_32_7_a18/

[1] Nevzorov F. F., Mamaev B. I., Isakov S, N., Tugushev N. U., “Raschet obtekaniya reshetok turbinnykh profilei szhimaemym potokom”, Proektirovanie i dovodka aviats. gazoturbinnykh dvigatelei, KuAI, Kuibyshev, 1981, 73–82

[2] Stepanov G. Yu., Gidrodinamika reshetok turbomashin, Fizmatgiz, M., 1962

[3] Aronov B. M., Mamaev B. I., “Opredelenie ugla vykhoda potoka gaza iz ploskoi turbinnoi reshetki profilei”, Izv. vuzov. Aviats. tekhn., 1964, no. 1, 75–84

[4] Zhukovskii M. I., Raschet obtekaniya reshetok profilei turbomashin, Mashgiz, M.–L., 1960