Experimental Investigation on Aerodynamic Characteristics of Statics and Dynamics of 76°-40° Double Delta Wing at High Angle of Attack
碩士 === 國立中興大學 === 機械工程學系 === 94 === This study is to investigate the high pitch flow field and aerodynamic characteristics of 76°- 40° double delta wing model in static and dynamic situation by employing water tunnel. The experiment is to measure vortex burst position and relevant forces with sides...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2006
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| Online Access: | http://ndltd.ncl.edu.tw/handle/30735516036754351365 |