caa a22 4500 469101504 CHVBK 20180323133045.0 cr unu---uuuuu 170328e19920301xx s 000 0 eng 10.1007/BF01052092 doi (NATIONALLICENCE)springer-10.1007/BF01052092 Method of determining the aerodynamic coefficients of asymmetric bodies with allowance for nonlinear body shape influence factors [Elektronische Daten] [G. Skiba, V. Yurov] The numerical method proposed makes it possible to determine the aerodynamic coefficients of asymmetric bodies of fairly arbitrary shape (including those with discontinuities of the transverse contour) at small solid angles of attack. The method allows an aerodynamically sound transition from the three-dimensional system of equations of gas dynamics to a two-dimensional system, which considerably simplifies the problem and reduces by an order the machine time required. The method takes into account the nonlinear body shape influence factors, which substantially improves the accuracy of the calculations. The efficiency and accuracy of the method are demonstrated by comparing the results of the calculations with the results of a numerical solution of the three-dimensional problem. Plenum Publishing Corporation, 1992 Skiba G. Moscow aut Yurov V. Moscow aut Fluid Dynamics Kluwer Academic Publishers-Plenum Publishers 27/2(1992-03-01), 245-250 0015-4628 27:2<245 1992 27 10697 https://doi.org/10.1007/BF01052092 text/html Onlinezugriff via DOI 1 research-article jats NATIONALLICENCE 856 40 https://doi.org/10.1007/BF01052092 text/html Onlinezugriff via DOI NATIONALLICENCE 700 1- Skiba G. Moscow aut NATIONALLICENCE 700 1- Yurov V. Moscow aut NATIONALLICENCE 773 0- Fluid Dynamics Kluwer Academic Publishers-Plenum Publishers 27/2(1992-03-01), 245-250 0015-4628 27:2<245 1992 27 10697 Metadata rights reserved Springer special CC-BY-NC licence nationallicence BK010053 XK010053 XK010000 NATIONALLICENCE NATIONALLICENCE NL-springer