BISPECTRAL ANALYSIS OF NUMERICAL SIMULATIONS OF WAVE PROCESSES IN HYPERSONIC SHOCK LAYERS

D. A. Bountin; A. A. Maslov; S. G. Mironov; T. V. Poplavskaya; I. S. Tsyryulnikov

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BISPECTRAL ANALYSIS OF NUMERICAL SIMULATIONS OF WAVE PROCESSES IN HYPERSONIC SHOCK LAYERS

机译：超音速激波层波过程数值模拟的双目分析

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摘要

Results of numerical simulations of the evolution of disturbances in a hypersonic shock layer on a flat plate at high Mach numbers (M_∞ = 21) and moderate Reynolds numbers (Re_L = 1.44 · 10~5) 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.

机译：通过改进的双谱分析方法，分析了高马赫数（M_∞= 21）和中等雷诺数（Re_L = 1.44·10〜5）时平板上高超声速冲击层扰动演变的数值模拟结果。。获得了非线性相互作用的所有基本类型。将计算结果与实验数据进行比较。

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《Journal of Applied Mechanics and Technical Physics》 |2012年第1期|p.1-8|共8页
作者
D. A. Bountin; A. A. Maslov; S. G. Mironov; T. V. Poplavskaya; I. S. Tsyryulnikov;
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作者单位

Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch, Russian Academy of Sciences, Novosibirsk, 630090 Russia Novosibirsk State University, Novosibirsk, 630090 Russia;

Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch, Russian Academy of Sciences, Novosibirsk, 630090 Russia Novosibirsk State University, Novosibirsk, 630090 Russia;

Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch, Russian Academy of Sciences, Novosibirsk, 630090 Russia Novosibirsk State University, Novosibirsk, 630090 Russia;

Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch, Russian Academy of Sciences, Novosibirsk, 630090 Russia Novosibirsk State University, Novosibirsk, 630090 Russia;

Khristianovich Institute of Theoretical and Applied Mechanics, Siberian Branch, Russian Academy of Sciences, Novosibirsk, 630090 Russia Novosibirsk State University, Novosibirsk, 630090 Russia;

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正文语种 eng
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关键词
hypersonic flows; shock layer; receptivity; direct numerical simulation; experiment; bispectral analysis;

机译：高超音速流;冲击层接受能力直接数值模拟;实验;双光谱分析;

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1. Bispectral Analysis of Nonlinear Processes in the Hypersonic Boundary Layer on a Porous Cone Surface [J] . D. A. Buntin, A. A. Maslov, T. A. Chimytov, Fluid Dynamics . 2010,第3期

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4. Uncertainty Assessments of 2D and Axisymmetric Hypersonic Shock Wave - Turbulent Boundary Layer Interaction Simulations at Compression Corners [C] . Peter A. Gnoffo, Scott A. Berry, John W. Van Norman AIAA thermophysics conference . 2011

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5. Numerical simulation of oblique detonation and shock-deflagration waves with a laminar boundary layer. [D] . Chuck, Chen. 1990

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6. Structural Change in Lipid Bilayers and Water Penetration Induced by Shock Waves: Molecular Dynamics Simulations [O] . Kenichiro Koshiyama, Tetsuya Kodama, Takeru Yano, 2006

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BISPECTRAL ANALYSIS OF NUMERICAL SIMULATIONS OF WAVE PROCESSES IN HYPERSONIC SHOCK LAYERS

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