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Influence of the sound-absorbing coating structure on the disturbance evolution in the hypersonic flow of vibrationally excited gases

机译：吸音涂层结构对振动激发气体过度流动扰动演化的影响

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A. I. Reshetova; T. V. Poplavskaya; I. S. Tsyrulnikov; O. V. Soloveva; S. V. Kirilovskiy;
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1. Influence of sound-absorbing coatings on the development of disturbances in a flowing mixture of vibrationally excited gases [J] . T.V. Poplavskaya, A.I. Reshetova, I.S. Tsyryulnikov Thermophysics and Aeromechanics . 2019,第3期

机译：吸音涂层对振动激发气体流动混合物开发的影响
2. The efficiency of the method of sound-absorbing coatings in vibrationally excited hypersonic flow [J] . Tsyryulnikov I. S., Maslov A. A., Mironov S. G., Technical physics letters: Letters to the Russian journal of applied physics . 2015,第2期

机译：振动激发高超音速流中吸声涂层方法的效率
3. Evolution of disturbances in the shock layer on a flat plate in the flow of a mixture of vibrationally excited gases [J] . S.V. Kirilovskiy, T.V. Poplavskaya, I.S. Tsyryulnikov, Thermophysics and Aeromechanics . 2017,第3期

机译：振动激发气体混合物流动中扁平板上的冲击层中的扰动的演变
4. Influence of the sound-absorbing coating structure on the disturbance evolution in the hypersonic flow of vibrationally excited gases [C] . A. I. Reshetova, T. V. Poplavskaya, I. S. Tsyrulnikov, International Conference on the Methods of Aerophysical Research . 2018

机译：吸音涂层结构对振动激发气体过度流动扰动演化的影响
5. Vibrational energy transfer of diatomic gases in hypersonic expanding flows. [D] . Ruffin, Stephen Merrick. 1993

机译：高超声速膨胀流中双原子气体的振动能量转移。
6. Chemical Dynamics Special Feature: Chemical dynamics of vibrationally excited molecules: Controlling reactions in gases and on surfaces [O] . F. Fleming Crim 2008

机译：化学动力学特性：振动激发分子的化学动力学：控制气体和表面上的反应
7. Numerical Investigation of the Evolution of Disturbances on a Flat Plate in a Hypersonic Flow of a Mixture of Vibrationally Excited Gases [O] . A. I. Reshetova, T. V. Poplavskaya 2017

机译：振动激发气体混合物过度流动下平板扰动紊乱演化的数值研究
8. Modeling Vortex-Excited Vibrations of Axially Varying Cylindrical Structures in Non-Uniform Flow Fields [R] . Skop, R. A. 1998

机译：非均匀流场中轴向变化圆柱结构的涡激振动模拟

Influence of the sound-absorbing coating structure on the disturbance evolution in the hypersonic flow of vibrationally excited gases

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