Optimization for the Aeroelastic Divergence of Composite Wing Structures
碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 90 === In subsonic speed, the aircrafts with high aspect ratio wing and forward swept wing may have superior aerodynamic performance and agile control, but it exists divergence problem. We define the higher divergence speed as the better performance to against dive...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2002
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| Online Access: | http://ndltd.ncl.edu.tw/handle/y9mjy5 |