caa a22 4500 469101539 CHVBK 20180323133045.0 cr unu---uuuuu 170328e19920301xx s 000 0 eng 10.1007/BF01052091 doi (NATIONALLICENCE)springer-10.1007/BF01052091 Numerical modeling of supersonic flow over wings with varying aspect ratio on a broad range of angles of attack using the law of plane sections [Elektronische Daten] [N. Voevodenko, I. Panteleev] A method and a program based on it for solving the problem of flow in the neighborhood of bodies of different shapes introduced into a high-supersonic stream at arbitrary angles of attack are proposed. The equations of the law of plane sections are integrated by Godunov's method. It is shown that the region of applicability of Sychev's theory is much broader than indicated in [1]. Plenum Publishing Corporation, 1992 Voevodenko N. Moscow aut Panteleev I. Moscow aut Fluid Dynamics Kluwer Academic Publishers-Plenum Publishers 27/2(1992-03-01), 239-244 0015-4628 27:2<239 1992 27 10697 https://doi.org/10.1007/BF01052091 text/html Onlinezugriff via DOI 1 research-article jats NATIONALLICENCE 856 40 https://doi.org/10.1007/BF01052091 text/html Onlinezugriff via DOI NATIONALLICENCE 700 1- Voevodenko N. Moscow aut NATIONALLICENCE 700 1- Panteleev I. Moscow aut NATIONALLICENCE 773 0- Fluid Dynamics Kluwer Academic Publishers-Plenum Publishers 27/2(1992-03-01), 239-244 0015-4628 27:2<239 1992 27 10697 Metadata rights reserved Springer special CC-BY-NC licence nationallicence BK010053 XK010053 XK010000 NATIONALLICENCE NATIONALLICENCE NL-springer