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This article is cited in 2 scientific papers (total in 2 papers)
Supersonic gas flows in radial nozzles
S. P. Kiselevab, V. P. Kiseleva, V. N. Zaikovskiia a Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch of the Russian Academy of Sciences, Novosibirsk, 630090, Russia
b Novosibirsk State Technical University, Novosibirsk, 630092, Russia
Abstract:
Results of experimental investigations and numerical simulations of supersonic gas flows in radial nozzles with different nozzle widths are presented. It is demonstrated that different types of the flow are formed in the nozzle with a fixed nozzle radius and different nozzle widths: supersonic flows with oblique shock waves inducing boundary layer separation are formed in wide nozzles, and flows with a normal pseudoshock separating the supersonic and subsonic flow domains are formed in narrow nozzles (micronozzles). The pseudoshock structure is studied, and the total pressure loss in the case of the gas flow in a micronozzle is determined.
Keywords:
radial nozzle, supersonic flow, pseudoshock, boundary layer, numerical simulation, experiment.
Received: 07.11.2016
Citation:
S. P. Kiselev, V. P. Kiselev, V. N. Zaikovskii, “Supersonic gas flows in radial nozzles”, Prikl. Mekh. Tekh. Fiz., 58:6 (2017), 78–90; J. Appl. Mech. Tech. Phys., 58:6 (2017), 1021–1032
Linking options:
https://www.mathnet.ru/eng/pmtf641 https://www.mathnet.ru/eng/pmtf/v58/i6/p78
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