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Interaction of long-wave perturbations with a shock wave on a wedge and method of mode decomposition of supersonic flow pulsations

机译：超声波流量脉动楔形楔对冲击波的长波扰动的相互作用及模式分解方法

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I S Tsyryulnikov; S V Kirilovskiy; T V Poplavskaya;
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1. Self-induced oscillations in the shock wave flow pattern formed in a stationary supersonic flow over a double wedge [J] . Ben-Dor G., Vasilev EI., Elperin T., Physics of fluids . 2003,第12期

机译：在双楔形上的固定超音速流中形成的冲击波流型中的自激振荡
2. Turbulence model assessment for shock wave/turbulent boundary-layer interaction in transonic and supersonic flows [J] . William W. Liou, George Huang, Tsan-Hsing Shih Computers & Fluids . 2000,第3期

机译：跨音速和超音速流动中冲击波/湍流边界层相互作用的湍流模型评估
3. NONLINEAR INTERACTION BETWEEN A PAIR OF OBLIQUE MODES IN A SUPERSONIC MIXING LAYER - LONG-WAVE LIMIT [J] . Gartside J., Balsa TF. Studies in Applied Mathematics . 1996,第1期

机译：超音速混合层中一对斜模之间的非线性相互作用-长波极限
4. Interaction of long-wave perturbations with a shock wave on a wedge and method of mode decomposition of supersonic flow pulsations [C] . I S Tsyryulnikov, S V Kirilovskiy, T V Poplavskaya All-Russian Conference with International Participation on Modern Problems of Continuum Mechanics and Explosion Physics . 2017

机译：超声波流量脉动楔形楔对冲击波的长波扰动的相互作用及模式分解方法
5. AN EXPERIMENTAL INVESTIGATION OF SHOCK WAVES AND TURBULENT BOUNDARY LAYER INTERACTIONS IN A SUPERSONIC FLOWFIELD THROUGH AN ANNULAR DUCT (SCRAMJET). [D] . STOCKBRIDGE, RICHARD DREXEL. 1986

机译：通过环形管道（SCRAMJET）进行超音速流场中冲击波和湍流边界层相互作用的实验研究。
6. Investigations on the complex flows induced by dual-swept/dual-ramp wedges in supersonic flows [O] . X. Gao, G. X. Xiang, W. J. Tang, -1

机译：超音速流中双扫/双斜坡楔引起的复流研究
7. Supersonic flow onto solid wedges, multidimensional shock waves and free boundary problems [O] . Chen, Gui-Qiang 2017

机译：超音速流到固体楔块上，多维冲击波和自由边界问题
8. Supersonic Inviscid Flows With Three-Dimensional Interaction of Shock Waves in Corners Formed by Intersecting Wedges [R] . Goonko, Y. P. , Kudryavtsev, A. N. , Rakhimov, R. D. 2002

机译：具有相交楔形成的角落中冲击波的三维相互作用的超音速非线性流动

Interaction of long-wave perturbations with a shock wave on a wedge and method of mode decomposition of supersonic flow pulsations

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