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Keyword [Shock-induced Boundary Layer Separation]
Result: 1 - 2 | Page: 1 of 1
1.
The Study Of Separated Flow Modeling And Unstart Mechanism Of Hypersonic Inlet
2.
Investigation On The Organization Method Of Passage Shock Wave And Control Of Leading-Edge Passage Shock Wave/Boundary-Layer Interaction Within “Shock-in-Type” Supersonic Compressor
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