Investigation of the Planar Shock Reflection–to–Diffraction on a Wedge with a Vertical Fin
碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 92 === The study of normal shock wave reflected on the wedges of 50° and 35°,respectively,with an overhanging vertical fin with incident shock Mach number of 1.30 to 1.69 has been done in the shock tube facility of Institute of Aeronautics and Astronautics in Nat...
Main Authors: | , |
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Other Authors: | |
Format: | Others |
Language: | zh-TW |
Published: |
2004
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Online Access: | http://ndltd.ncl.edu.tw/handle/57922224872457570980 |