Experiments on the Vibration Attenuation of Homeycomb Sandwich Panels Using MFC Actuators
碩士 === 大葉大學 === 機械工程研究所碩士班 === 96 === New all-composite aircraft fuselage designs are being developed with a flexible honeycomb core sandwiched between carbon fiber reinforced composite laminate face sheets. The honeycomb sandwich panels offer potential advantages for significant weight reduction,...
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| Format: | Others |
| Language: | zh-TW |
| Published: |
2008
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| Online Access: | http://ndltd.ncl.edu.tw/handle/14347609934001431352 |