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Volumn 24, Issue 2-4, 2002, Pages 273-279

Spectrum fatigue of composite bolted joints

Author keywords

Bolted joints; Composites; Flight simulation fatigue; Linear damage summation; S N curves

Indexed keywords

AIRCRAFT MATERIALS; BOLTED JOINTS; COMPOSITE STRUCTURES; FATIGUE TESTING;

EID: 0036144230     PISSN: 01421123     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0142-1123(01)00082-2     Document Type: Article
Times cited : (28)

References (18)
  • 1
    • 0000800257 scopus 로고
    • The development of fatigue damage around fastener holes in thick graphite/epoxy composite laminates
    • (1993) Composites , vol.24 , pp. 309-321
    • Saunders, D.S.1
  • 3
    • 0020497922 scopus 로고
    • Fatigue spectrum sensitivity of composite joints
    • (1983) Composites , vol.14 , pp. 27-33
    • Demuts, E.1
  • 4
    • 84914929399 scopus 로고
    • Bolted joint design
    • Test Methods and Design Allowables for Fibrous Composites
    • (1981) ASTM STP , vol.734 , pp. 376-395
    • Ramkumar, R.L.1
  • 10
    • 85122696944 scopus 로고
    • Effects of truncation of a predominantly compression load spectrum on the life of a notched graphite/epoxy laminate
    • Fatigue of Fibrous Composite Materials, American Society for Testing and Materials
    • (1981) ASTM STP , vol.723 , pp. 197-212
    • Phillips, E.P.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.