Investigations of wake flow of a circular cylinder in the critical regime by MEMS film sensors array
碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 96 === An experimental investigation of flow around a smooth circular cylinder was carried out in a transonic wind tunnel,at Reynolds numbers 4.1x105~5.67x105,corresponding the Mach numbers in a range of 0.4 to 0.7. Unsteady characteristics of flow separation were...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2008
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| Online Access: | http://ndltd.ncl.edu.tw/handle/15000169017029822366 |