Analysis of the shock wave/transitional boundary layer interaction at Mach 5

B. CHANETZ; R. BENAY

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Analysis of the shock wave/transitional boundary layer interaction at Mach 5

机译：5马赫冲击波/过渡边界层相互作用的分析

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An experimental study of the shock wave / tran- sitional boundary interaction was carried out in the R2Ch hypersonic wind tunnel at Mach number 5 on an axisymmetric cylinder-flare model. This problem concerns applications of not only the PRE-X programme type atmospheric re-entry vehicle but also the FLPP (Future Launcher Preliminary Programme) type programmes, concerning future launchers, of which it is a priority task.

机译：在轴对称圆柱扩口模型上，在马赫数为5的R2Ch高超声速风洞中进行了冲击波/横向边界相互作用的实验研究。这个问题不仅涉及PRE-X程序型大气再入飞行器的应用，而且还涉及涉及未来发射器的FLPP（未来发射器初步程序）类型的程序，这是首要任务。

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《ONERA Scientific and Technical Activities》 |2005年第2005期|p.26|共1页
作者
B. CHANETZ; R. BENAY;
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1. Analysis of the two-dimensional dynamics of a Mach 1.6 shock wave/transitional boundary layer interaction using a RANS based resolvent approach [J] . Bonne N., Brion V, Garnier E., Journal of Fluid Mechanics . 2019,第期

机译：基于RAN的解析方法分析马赫1.6冲击波/过渡边界层相互作用的二维动力学
2. Experiments on transitional shock wave - Boundary layer interactions at Mach 5 [J] . Erdem E., Kontis K., Johnstone E., Experiments in Fluids: Experimental Methods and Their Applications to Fluid Flow . 2013,第10期

机译：5马赫过渡冲击波-边界层相互作用实验。
3. The influence of the laminar-turbulent transition on the interaction between the shock wave and boundary layer at a low supersonic Mach number [J] . Polivanov P. A., Sidorenko A. A., Maslov A. A. Technical physics letters: Letters to the Russian journal of applied physics . 2015,第10期

机译：低超声速马赫数下层流湍流对冲击波与边界层相互作用的影响
4. Exploration of Upstream Influence and the Role of Shock Generator Geometry in Shock Wave/Transitional Boundary Layer Interactions at Mach 1.8 Edge Conditions [C] . E. Lara Lash, Mark Gragston, Zachary McDaniel, AIAA Aviation Forum . 2020

机译：探讨上游影响和冲击发生器几何在马赫1.8边缘条件下冲击波/过渡边界层相互作用中的作用
5. Physics of unsteady cylinder-induced transitional shock wave boundary layer interactions. [D] . Murphree, Zachary Ryan. 2009

机译：非定常圆柱引起的过渡冲击波边界层相互作用的物理学。
6. Interaction between shock wave and single inertial bubbles near an elastic boundary [O] . G. N. Sankin, P. Zhong -1

机译：冲击波与弹性边界附近的单个惯性气泡之间的相互作用
7. Interaction between shock waves and turbulent or transitional boundary layers at mach number 3. [O] . Irish Edelbert E. 1957

机译：马赫数为3时，冲击波与湍流或过渡边界层之间的相互作用。

Analysis of the shock wave/transitional boundary layer interaction at Mach 5

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