Finite element analysis of cohesive element for glass epoxy composite fuselage model

In this research, a numerical simulation on a newly introduced fabrication miniature composite fuselage structure - a glass epoxy composite laminated with adhesively bonded butt joint under axial compression loading is presented. A FEA via ABAQUS/Explicit is utilized to capture the complete compress...

詳細記述

書誌詳細

第一著者:	Ng, Wei Sim
フォーマット:	学位論文
言語:	英語
出版事項:	2011
主題:	Finite element method (Engineering analysis) Laminated materials
オンライン･アクセス:	http://psasir.upm.edu.my/id/eprint/41770/1/FK%202011%202R.pdf