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Skin Friction Reduction of Hypersonic Body by Supersonic Layer |
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| Authors: | Zhao X H Yi S H Mi Q Hu Y F Ding H L |
| Institution: | 1.College of Aerospace Science and Engineering, National University of Defense Technology, Changsha, Hunan, China ; |
| Abstract: | Fluid Dynamics - Both numerical methods and wind tunnel tests were used to reduce skin friction for a hypersonic body. A hypersonic cone was tested under three different free-stream flow... |
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