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Volumn 15, Issue 10, 2001, Pages 1247-1259

A stress singularity approach to failure initiation in a bonded joint with varying bondline thickness

Author keywords

Interface stresses; Optimum bondline thickness; Single lap joint; Stress intensity factor; Stress singularity

Indexed keywords

BONDING; CALCULATIONS; CONTINUUM MECHANICS; FAILURE (MECHANICAL); FINITE ELEMENT METHOD; FRACTURE MECHANICS; INTERFACES (MATERIALS); STRESS INTENSITY FACTORS; STRESSES; THICKNESS MEASUREMENT;

EID: 0035170206     PISSN: 01694243     EISSN: None     Source Type: Journal    
DOI: 10.1163/156856101317048734     Document Type: Article
Times cited : (29)

References (13)
  • 7
    • 4243395422 scopus 로고    scopus 로고
    • Crack growth simulation and residual strength prediction in airplane fuselages
    • NASA March
    • C. Chen, P. A. Wawrzynek and A. R. Ingraffea, Crack growth simulation and residual strength prediction in airplane fuselages - Technical Report CR-1999-209115, NASA (March 1999).
    • (1999) Technical Report , vol.CR-1999-209115
    • Chen, C.1    Wawrzynek, P.A.2    Ingraffea, A.R.3


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.