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  5. Numerical Study on Flow Separation of Shock Train in a Planar Rectangular Duct

Numerical Study on Flow Separation of Shock Train in a Planar Rectangular Duct

来源 :第14届亚洲显示会议(The 14th Asian Symposium on Visualization) | 被引量 : 0次 | 上传用户：pww030
【摘 要】
：
The interaction between a shock wave and a boundary layer along a duct wall forms very complicated flow structures characterized by shock train.
【作 者】
：
Pei Chen Suxun Li 
【机 构】
：
China Academy of Aerospace Aerodynamics,100074,Beijing,China
【出 处】
：
第14届亚洲显示会议(The 14th Asian Symposium on Visualization)
【发表日期】
：
2017年11期
【关键词】
：
shock train shock boundary layer interaction flow confinement numerical simulati 
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　　The interaction between a shock wave and a boundary layer along a duct wall forms very complicated flow structures characterized by shock train.
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