Aeroelastic Divergence of Composite Wing Structures
碩士 === 國立成功大學 === 航空太空工程學系 === 88 === Divergence of wing structures is an important topic in aeroelasticity. In present work the aeroelastic model of composite wing is established by employing the theory of composite sandwich beams. Transverse shear effect will be considered in our study....
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2000
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| Online Access: | http://ndltd.ncl.edu.tw/handle/53484053929443454809 |