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Volumn 32, Issue 2, 2003, Pages 65-70

Finite element analysis of effects of clearance on single shear composite bolted joints

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; BOUNDARY CONDITIONS; BUCKLING; COMPOSITE MATERIALS; COMPUTER SIMULATION; DELAMINATION; EPOXY RESINS; FINITE ELEMENT METHOD; GRAPHITE; STIFFNESS;

EID: 1442282648     PISSN: 14658011     EISSN: None     Source Type: Journal    
DOI: 10.1179/146580103225001390     Document Type: Conference Paper
Times cited : (51)

References (13)
  • 3
    • 84892977481 scopus 로고
    • Bearing bypass loading on bolted composite joints
    • National Aeronautics and Space Administration. Washington DC; May
    • J. H. CREWS and R. A. NAIK: Bearing bypass loading on bolted composite joints, Report NASA TM 89153, National Aeronautics and Space Administration. Washington DC; May 1987.
    • (1987) Report NASA TM 89153
    • Crews, J.H.1    Naik, R.A.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.