Experimental and Numerical Simulation Research on Boundary Layer Transition Front over a Swept Wing at M = 6 |
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| Authors: | Zhang F Yi S H Niu H B Lu X G Wang X X |
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| Institution: | 1.College of Aerospace Science and Engineering, National University of Defense Technology, 410073, Changsha, Hunan, China
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| Abstract: | Fluid Dynamics - To predict the boundary layer transition on swept wings, experimental and numerical researches were conducted to obtained the accurate boundary layer transition front and to... |
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