A Study of Crushing Behavior of Aluminum Honeycombs Subjected to Axial Impact Loading Test
碩士 === 國立成功大學 === 航空太空工程學系 === 102 === SUMMARY The major purpose of this research is to investigate the dynamic impact response of aluminum honeycomb structure subjected to an axial impact loading. The explicit solver of FEM software LS-DYNA is used in current simulation. First, through the compari...
| Main Authors: | , |
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| Other Authors: | |
| Format: | Others |
| Language: | zh-TW |
| Published: |
2014
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| Online Access: | http://ndltd.ncl.edu.tw/handle/53949244285468515942 |