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Prikladnaya Mekhanika i Tekhnicheskaya Fizika, 2002, Volume 43, Issue 6, Pages 100–112
(Mi pmtf2695)
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This article is cited in 3 scientific papers (total in 3 papers)
Experimental and numerical study of a hypersonic separated flow in the vicinity of a cone-flare model
I. A. Bedarev, A. A. Maslov, A. A. Sidorenko, N. N. Fedorova, A. N. Shiplyuk Institute of Theoretical and Applied Mechanics, Siberian Division, Russian Academy of Sciences, Novosibirsk, 630090
Abstract:
An axisymmetric laminar separated flow in the vicinity of a cone-flare model is studied experimentally and numerically for a Mach number $\mathrm{M} = 6$. The distributions of pressure and Stanton numbers along the model surface and velocity profiles in the region of shock wave–boundary layer interaction are measured and compared with the calculated data. The influence of the laminar–turbulent transition on flow parameters is studied numerically.
Received: 29.04.2002
Citation:
I. A. Bedarev, A. A. Maslov, A. A. Sidorenko, N. N. Fedorova, A. N. Shiplyuk, “Experimental and numerical study of a hypersonic separated flow in the vicinity of a cone-flare model”, Prikl. Mekh. Tekh. Fiz., 43:6 (2002), 100–112; J. Appl. Mech. Tech. Phys., 43:6 (2002), 867–876
Linking options:
https://www.mathnet.ru/eng/pmtf2695 https://www.mathnet.ru/eng/pmtf/v43/i6/p100
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