Optimum Design of Helicopter Rotor Blade by Response Surface Methodology
碩士 === 淡江大學 === 航空太空工程學系碩士班 === 93 === This study presents an application of Response Surface Methodology (RSM) for a helicopter rotor blade design through an unsteady wake dynamic and aerodynamic coupling system. The purpose of this study is to obtain the optimal configuration of the blade which to...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2005
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| Online Access: | http://ndltd.ncl.edu.tw/handle/21715930665472982362 |