Scaling of Upstream Influence Line Induced by Shock Sweeping Concave Half-Cylinder
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Veröffentlicht in: | AIAA journal 2024-07, Vol.62 (7), p.2800-2808 |
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container_title | AIAA journal |
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creator | Huang, Qi Hong, Yuting Li, Zhufei |
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doi_str_mv | 10.2514/1.J063924 |
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Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at ; employ the eISSN to initiate your request. See also AIAA Rights and Permissions .</rights><rights>Copyright © 2024 by the authors. Published by the American Institute of Aeronautics and Astronautics, Inc., with permission. All requests for copying and permission to reprint should be submitted to CCC at www.copyright.com; employ the eISSN 1533-385X to initiate your request. 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source | Alma/SFX Local Collection |
subjects | Boundary conditions Finite volume method Geometry Influence lines Mechanics Reynolds number Symmetry Turbulence models |
title | Scaling of Upstream Influence Line Induced by Shock Sweeping Concave Half-Cylinder |
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