Analysis of wing structures with vertical takeoff and landing and rapid horizontal flight vehicle
碩士 === 建國科技大學 === 自動化工程系暨機電光系統研究所 === 106 === In this paper, HYPERMESH∕LS-DYNA finite element analysis method was used, and the structural strength of the wing structures were predicted. Flight conditions of the vehicles were analyzed at 0, 30, 60, and 90 degrees and the strength analyzed from four...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2018
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| Online Access: | http://ndltd.ncl.edu.tw/handle/3c73pu |