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,...

Full description

Bibliographic Details
Main Authors: Kai Lin WU, 吳鎧麟
Other Authors: J. J. RO
Format: Others
Language:zh-TW
Published: 2008
Online Access:http://ndltd.ncl.edu.tw/handle/79690831980565069067