An Experimental Study on a compressible Cylindrical cavity Flow
碩士 === 國立成功大學 === 航空太空工程學系 === 106 === This study aims to characterize the effect of incoming boundary layer thickness, diameter, depth and Mach number on a compressible, cylindrical cavity flow. The ratio of cavity diameter and depth, D/h, varies from 3.22 to 43.00 and the ratio of boundary layer t...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2018
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| Online Access: | http://ndltd.ncl.edu.tw/handle/9cg6t2 |