caa a22 4500 469100141 CHVBK 20180323133042.0 cr unu---uuuuu 170328e19920101xx s 000 0 eng 10.1007/BF01054181 doi (NATIONALLICENCE)springer-10.1007/BF01054181 Markov A. Moscow aut Unsteady viscous shock layer in the case of supersonic motion through an inhomogeneity [Elektronische Daten] [A. Markov] The model of a perfect gas is used in a numerical simulation of unsteady effects in a viscous shock layer near the stagnation streamline near the front part of a rotating blunt body in an inhomogeneous external flow with pressure difference ΔP t8, temperature difference ΔT t8, and vorticity difference ΔΩ. The evolution of nonlinear disturbances due to the passage of a heated region and a change of the injection regime is followed. A divergence finite-difference scheme of second order of approximation across the shock layer, realized by vector sweeps with allowance for the boundary conditions on the surface of the body and behind the separated bow shock wave, is used. Plenum Publishing Corporation, 1992 Fluid Dynamics Kluwer Academic Publishers-Plenum Publishers 27/1(1992-01-01), 104-109 0015-4628 27:1<104 1992 27 10697 https://doi.org/10.1007/BF01054181 text/html Onlinezugriff via DOI 1 research-article jats NATIONALLICENCE 856 40 https://doi.org/10.1007/BF01054181 text/html Onlinezugriff via DOI NATIONALLICENCE 100 1- Markov A. Moscow aut NATIONALLICENCE 773 0- Fluid Dynamics Kluwer Academic Publishers-Plenum Publishers 27/1(1992-01-01), 104-109 0015-4628 27:1<104 1992 27 10697 Metadata rights reserved Springer special CC-BY-NC licence nationallicence BK010053 XK010053 XK010000 NATIONALLICENCE NATIONALLICENCE NL-springer