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SELF-INDUCED OSCILLATIONS IN THE SHOCK WAVE FLOW PATTERN FORMED IN A STATIONARY SUPERSONIC FLOW OVER A DOUBLE WEDGE -A NUMERICAL INVESTIGATION

机译：双楔楔形超音速流动形成的激波流型中的自激振荡-数值研究

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Numerical simulations of a two-dimensional supersonic flow of an inviscid perfect gas over adouble wedge in the Mach numbers range 5 ≤ M ≤ 9, revealed the existence of self-inducedoscillations in the shock wave flow in a narrow range of geometrical parameters.

机译：马赫数范围为5≤M≤9的双楔形上无粘性完美气体的二维超声速流动的数值模拟表明，在狭窄的几何参数范围内，冲击波流中存在自激振荡。

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《Israel Annual Conference on Aerospace Sciences》|2004年|p.1-9|共9页
会议地点 Israel(IL)
作者
Gabi Ben-Dor; Tov Elperin; Eugene I. Vasilev; Andrew.V. Zenovich;
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Pearlstone Center for Aeronautical Engineering Studies Department of Mechanical Engineering Ben-Gurion University of the Negev Beer Sheva 84105 Israel e-mail: bendorg@bgumail.bgu.ac.il;

Pearlstone Center for Aeronautical Engineering Studies Department of Mechanical Engineering Ben-Gurion University of the Negev Beer Sheva 84105 Israel;

Department of Computational Mechanics Volgograd State University Volgograd Russia e-mail: vasil-ei@vlink.ru;

Department of Computational Mechanics Volgograd State University Volgograd Russia;

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专利

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. Numerical study of the oscillations induced by shock/shock interaction in hypersonic double-wedge flows [J] . Z. M. Hu, R. S. Myong, C. Wang, Shock Waves . 2008,第1期

机译：高超音速双楔流激波/激波相互作用引起的振荡的数值研究
3. Numerical study of the oscillations induced by shock/shock interaction in hypersonic double-wedge flows [J] . Hu ZM, Myong RS, Wang C, Shock Waves . 2008,第1期

机译：高超声速双楔流激波/激波相互作用引起的振荡的数值研究
4. Numerical Simulation of Interaction of Long-Wave Disturbances with a Shock Wave on a Wedge for the Problem of Mode Decomposition of Supersonic Flow Oscillations [C] . S.V. Kirilovskiy, T.V. Poplavskaya, I.S. Tsyryulnikov International Conference on the Methods of Aerophysical Research . 2016

机译：超声波流动振荡模式分解楔对楔形冲击波的长波扰动相互作用的数值模拟
5. An Optical Technique for Investigating Shock Oscillations in Supersonic Flows [D] . Alanzi, Abdulaziz 2019

机译：研究超音速流动中激波振荡的光学技术
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. Study on Supersonic Internal Flows with Shock Waves : Investigation by Numerical Analysis on the Internal Structure of Mach 2 Pseudo-Shock Wave in a Two-Dimensional Channel [O] . 孫立群, 杉山弘, 溝端一秀, 2003

机译：具有冲击波的超声内部流动研究 - 二维通道中mach 2伪激波的内部结构数值分析研究
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

SELF-INDUCED OSCILLATIONS IN THE SHOCK WAVE FLOW PATTERN FORMED IN A STATIONARY SUPERSONIC FLOW OVER A DOUBLE WEDGE -A NUMERICAL INVESTIGATION

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