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Volumn 94, Issue 6, 2012, Pages 2110-2117

On the prediction of bolted single-lap composite joints

Author keywords

Aeronautical structures; Bolted joint; Composite joint; Finite element modelling

Indexed keywords

AERONAUTICAL STRUCTURES; COMPARISON WITH EXPERIMENTS; COMPOSITE FAILURE; COMPOSITE JOINT; FAILURE CRITERIA; FINITE ELEMENT MODELLING; FINITE ELEMENT MODELS; FRICTION COEFFICIENTS; GEOMETRIC NON-LINEARITY; NON-LINEAR FINITE ELEMENT MODEL; OUT-OF-PLANE FAILURES; PARAMETRIC STUDY; PROGRESSIVE DAMAGE; SECONDARY BENDING; STRESS-STRAIN RELATIONSHIPS; THREE-DIMENSIONAL STRESS FIELD; TIGHTENING TORQUE;

EID: 84859501678     PISSN: 02638223     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.compstruct.2012.01.016     Document Type: Article
Times cited : (191)

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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.