caa a22 4500 469100990 CHVBK 20180323133044.0 cr unu---uuuuu 170328e19920701xx s 000 0 eng 10.1007/BF01051333 doi (NATIONALLICENCE)springer-10.1007/BF01051333 Influence of second-order boundary layer effects in hypersonic flow over slender blunt cones [Elektronische Daten] [D. Gan'zha, G. Tirskii, S. Utyuzhnikov, M. Fridlender] The aim of this study is to determine the influence of second-order effects in the aggregate on supersonic axisymmetric flow over slender blunt cones and also to determine the region of applicability of approximate methods of taking into account the strongest of these second-order effects — entropy layer absorption. A system of complete viscous shock layer equations containing all the terms of the gas dynamic Euler equations and all the second-order terms of asymptotic boundary layer theory is chosen as the gas-dynamic model. Within the calculation domain the problem is solved in a unified manner. Plenum Publishing Corporation, 1993 Gan'zha D. Moscow aut Tirskii G. Moscow aut Utyuzhnikov S. Moscow aut Fridlender M. Moscow aut Fluid Dynamics Kluwer Academic Publishers-Plenum Publishers 27/4(1992-07-01), 551-555 0015-4628 27:4<551 1992 27 10697 https://doi.org/10.1007/BF01051333 text/html Onlinezugriff via DOI 1 research-article jats NATIONALLICENCE 856 40 https://doi.org/10.1007/BF01051333 text/html Onlinezugriff via DOI NATIONALLICENCE 700 1- Gan'zha D. Moscow aut NATIONALLICENCE 700 1- Tirskii G. Moscow aut NATIONALLICENCE 700 1- Utyuzhnikov S. Moscow aut NATIONALLICENCE 700 1- Fridlender M. Moscow aut NATIONALLICENCE 773 0- Fluid Dynamics Kluwer Academic Publishers-Plenum Publishers 27/4(1992-07-01), 551-555 0015-4628 27:4<551 1992 27 10697 Metadata rights reserved Springer special CC-BY-NC licence nationallicence BK010053 XK010053 XK010000 NATIONALLICENCE NATIONALLICENCE NL-springer