Active Noise Control of Honeycomb 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,...
Main Authors: | Kai Lin WU, 吳鎧麟 |
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Other Authors: | J. J. RO |
Format: | Others |
Language: | zh-TW |
Published: |
2008
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Online Access: | http://ndltd.ncl.edu.tw/handle/79690831980565069067 |
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