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Prikladnaya Mekhanika i Tekhnicheskaya Fizika, 2012, Volume 53, Issue 1, Pages 3–11
(Mi pmtf1321)
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This article is cited in 1 scientific paper (total in 1 paper)
Bispectral analysis of numerical simulations of wave processes in hypersonic shock layers
D. A. Bountinab, A. A. Maslovab, S. G. Mironovab, T. V. Poplavskayaab, I. S. Tsyryulnikovab a Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch, Russian Academy of Sciences, Novosibirsk, 630090, Russia
b Novosibirsk State University
Abstract:
Results of numerical simulations of the evolution of disturbances in a hypersonic shock layer on a flat plate at high Mach numbers ($\mathrm{M}_\infty=21$) and moderate Reynolds numbers $(\operatorname{Re}_L=1,44\cdot10^5)$ are analyzed by an adapted method of bispectral analysis. All basic types of nonlinear interactions are obtained. The calculated results are compared with experimental data.
Keywords:
hypersonic flows, shock layer, receptivity, direct numerical simulation, experiment, bispectral analysis.
Received: 30.05.2011
Citation:
D. A. Bountin, A. A. Maslov, S. G. Mironov, T. V. Poplavskaya, I. S. Tsyryulnikov, “Bispectral analysis of numerical simulations of wave processes in hypersonic shock layers”, Prikl. Mekh. Tekh. Fiz., 53:1 (2012), 3–11; J. Appl. Mech. Tech. Phys., 53:1 (2012), 1–8
Linking options:
https://www.mathnet.ru/eng/pmtf1321 https://www.mathnet.ru/eng/pmtf/v53/i1/p3
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