Research and Discussion of Patching Aircraft Structure by Compound Material

碩士 === 大葉大學 === 工業工程與科技管理學系碩士在職專班 === 99 === This study is to explore the effectiveness of bonding factors for adhesive material and treatment by patching one-side composite material and touching up the test sample of metal structure, tests of structure fatigue and life durability will be conducted...

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Bibliographic Details
Main Authors: Lai,Fang-Chuan, 賴芳川
Other Authors: Lin,Char-Yuan
Format: Others
Language:zh-TW
Published: 2011
Online Access:http://ndltd.ncl.edu.tw/handle/16104143755874672448