首页> 外文会议>AIAA Fluid Dynamics Conference and Exhibit >Numerical Investigation of Flow Transition Caused by the Interaction of Oblique Shocks and Supersonic Boundary Layers

【24h】

Numerical Investigation of Flow Transition Caused by the Interaction of Oblique Shocks and Supersonic Boundary Layers

机译：斜激波与超音速边界层相互作用引起的流动过渡的数值研究

获取原文

页面导航

著录项
引文网络
相似文献
相关主题

著录项

来源
《AIAA Fluid Dynamics Conference and Exhibit》|2008年|P.1-14|共14页
会议地点 Seattle WA(US)
作者
J. Ekaterinaris;
展开▼
作者单位

University of Patras Patra Greece;

展开▼
会议组织
原文格式 PDF
正文语种
中图分类
关键词

相似文献

外文文献
中文文献
专利

1. Numerical Investigation of Transitional Shock-Wave/rnBoundary-Layer Interaction in Supersonic Regime [J] . Quadros Russell, Bernardini Matteo AIAA Journal . 2018,第7期

机译：超音速状态下过渡冲击波/ rn边界层相互作用的数值研究
2. Numerical investigations of shock wave interactions with a supersonic turbulent boundary layer [J] . Avinash Jammalamadaka, Zhaorui Li, Farhad Jaberi Physics of fluids . 2014,第5期

机译：超音速湍流边界层与激波相互作用的数值研究
3. Numerical simulations of shock-wave interaction with a boundary layer in the plane supersonic flows with jet injection [J] . Beketaeva A. O., Moisseyeva Ye S., Naimanova A. Zh Thermophysics and Aeromechanics . 2016,第2期

机译：平面超音速射流中边界层冲击波相互作用的数值模拟
4. Numerical Investigation of Flow Transition Caused by the Interaction of Oblique Shocks and Supersonic Boundary Layers [C] . American Institute of Aeronautics and Astronautics Fluid Dynamics Conference and Exhibit . 2008

机译：倾斜冲击与超声边界层相互作用引起的流动转变的数值研究
5. Investigation of Laser Discharge in a Supersonic Flow and Shock Wave Laminar Boundary Layer Interaction in a Hypersonic Flow [D] . Mortazavi Ravari, Mahsaalsadat. 2018

机译：超音速流中激光放电与高音速流中冲击波层流边界层相互作用的研究
6. Interaction of a Backward-Facing Step and Crossflow Instabilities in Boundary-Layer Transition [O] . Jenna L. Eppink, Richard W. Wlezien, Rudolph A. King, -1

机译：边界层过渡中向后步的相互作用和错流不稳定性
7. Interaction between Oblique Shock Waves and Boundary Layers in a Low-Pressure Supersonic Diffuser for Gas Dynamic Laser. [O] . Ken TAMURA, Tsunehisa SATAKE, Tomoyuki UCHIMURA, 1996

机译：倾斜冲击波与钢水型扩散器中的倾斜冲击波和边界层气体动力学激光器的相互作用。
8. Experimental and Numerical Investigation of the Effect of Distributed Suction on Oblique Shock Wave/Turbulent Boundary Layer Interaction. [R] . benhachmi, d. greber, i. 1988

机译：分布吸力对斜冲击波/湍流边界层相互作用影响的实验与数值研究。

Numerical Investigation of Flow Transition Caused by the Interaction of Oblique Shocks and Supersonic Boundary Layers

著录项

引文网络

相似文献

相关主题

期刊订阅