Thermal Buckling Analysis Of Composite Laminates

碩士 === 國立成功大學 === 航空太空工程學系碩博士班 === 91 === Subject :Thermal Buckling Analysis Of Composite Laminates Student :Cheng-Yuan Chen Adviser :Le-Chung Shiau In this thesis, by using the first order shear deformation plate theory, a 36 degree-of-freedom high precision, high order triangular plate eleme...

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Bibliographic Details
Main Authors: Cheng-Yuan Chen, 陳證元
Other Authors: Le-Chung Shiau
Format: Others
Language:zh-TW
Published: 2003
Online Access:http://ndltd.ncl.edu.tw/handle/68038952257236215420