Art

J-GLOBAL ID：202002246427688904   Reference number：20A0479789

Damage tolerance of CFRP airframe bolted joints in bearing, following bolt pull-through failure

軸受におけるCFRP機体ボルト接合部の損傷許容性【JST・京大機械翻訳】

Author (4)： Giannopoulos Ioannis K. (Centre of Excellence for Aeronautics, School of Aerospace, Transport and Manufacturing, Cranfield University, Cranfield, MK43 0AL, UK) ,  Grafton Kaelan (Centre of Excellence for Aeronautics, School of Aerospace, Transport and Manufacturing, Cranfield University, Cranfield, MK43 0AL, UK) ,  Guo Shijun (Centre of Excellence for Aeronautics, School of Aerospace, Transport and Manufacturing, Cranfield University, Cranfield, MK43 0AL, UK) ,  Smith Howard (Centre of Excellence for Aeronautics, School of Aerospace, Transport and Manufacturing, Cranfield University, Cranfield, MK43 0AL, UK)
Material： Composites. Part B. Engineering  (Compos Pt B Eng)
Volume： 185  Page： Null  Publication year： 2020 
JST Material Number： W0437B  ISSN： 1359-8368  Document type： Article
Article type： 原著論文  Country of issue： United Kingdom (GBR)  Language： ENGLISH (EN)

Abstract/Point： The experimental study present...

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Thesaurus term： *bolted joint ,  *bearing ,  residual strength ,  *airframe ,  structural joint ,  spectrum ,  air transportation ,  authentication ,  airworthiness ,  American Society for Testing and Materials ,  carbon fiber ,  *carbon fiber reinforced plastics ,  fiber reinforced plastic ,  laminated material
Semi thesaurus term： 初期破壊 , 【Automatic Indexing@JST】

Author keywords (4)： Structural joints ,  Mechanical testing ,  Strength ,  Damage tolerance

JST classification (2)： Molding of reinforced plastics  (YH04060J) ,  Connections  (HD03080V)

Terms in the title (5)： 軸受 ,  CFRP ,  機体 ,  ボルト接合部 ,  損傷許容性