Structure Design and Analysis of a Ultralight Airplane
碩士 === 國立屏東科技大學 === 車輛工程系所 === 97 === This research presents the structural design and analysis, including normal mode , structural stiffness and impact strength, for Ultralight Aircraft by using Finite Element Analysis (FEA). The finite element model of the full aircraft structure is established by...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2009
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| Online Access: | http://ndltd.ncl.edu.tw/handle/15472723371105715965 |