caa a22 4500 469101393 CHVBK 20180323133045.0 cr unu---uuuuu 170328e19920301xx s 000 0 eng 10.1007/BF01052085 doi (NATIONALLICENCE)springer-10.1007/BF01052085 Mixing enhancement behind an oblique shock wave [Elektronische Daten] [V. Vasil'ev, S. Zakotenko] The possibility of mixing enhancement when a design-condition cocurrent jet passes through a stationary oblique shock is investigated. In [4] the effect of such a shock on the mixing layer of flows with Mach numbers M = 3 and 5 was experimentally investigated and it was shown that behind the shock no turbulence is generated. However, irrespective of its effect on the turbulence characteristics, an oblique shock causes deformation of the jet, modifying its dimensions, and in the three-dimensional case the shape of the cross section. The effect of this deformation on mixing, which is shown to be fairly significant, has been investigated theoretically using a numerical method. An approximate relation describing the variation of the maximum admixture concentration in the jet behind the shock is proposed. Plenum Publishing Corporation, 1992 Vasil'ev V. Moscow aut Zakotenko S. Moscow aut Fluid Dynamics Kluwer Academic Publishers-Plenum Publishers 27/2(1992-03-01), 196-201 0015-4628 27:2<196 1992 27 10697 https://doi.org/10.1007/BF01052085 text/html Onlinezugriff via DOI 1 research-article jats NATIONALLICENCE 856 40 https://doi.org/10.1007/BF01052085 text/html Onlinezugriff via DOI NATIONALLICENCE 700 1- Vasil'ev V. Moscow aut NATIONALLICENCE 700 1- Zakotenko S. Moscow aut NATIONALLICENCE 773 0- Fluid Dynamics Kluwer Academic Publishers-Plenum Publishers 27/2(1992-03-01), 196-201 0015-4628 27:2<196 1992 27 10697 Metadata rights reserved Springer special CC-BY-NC licence nationallicence BK010053 XK010053 XK010000 NATIONALLICENCE NATIONALLICENCE NL-springer