Effect of delamination on flutter of composite laminated plates

碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 95 === The effect of delamination on the flutter boundary of a delaminated rectangular plate was investigated by Finite Strip Method. Linear structural theory, quasi-steady supersonic aerodynamic theory and a moving together model were empolyed for the analysis. Th...

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Bibliographic Details
Main Authors: Yueh-Feng Tsai, 蔡岳峯
Other Authors: Le-Chung Shiau
Format: Others
Language:zh-TW
Published: 2007
Online Access:http://ndltd.ncl.edu.tw/handle/97531651141343030010