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Volumn 38, Issue 1, 2002, Pages 37-51

Strain energy density prediction of fatigue crack growth from hole of aging aircraft structures

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT; DATA REDUCTION; FATIGUE OF MATERIALS; FINITE ELEMENT METHOD; MORPHOLOGY; STRAIN; STRESS INTENSITY FACTORS;

EID: 0036650335     PISSN: 01678442     EISSN: None     Source Type: Journal    
DOI: 10.1016/S0167-8442(02)00079-4     Document Type: Article
Times cited : (23)

References (29)
  • 7
    • 0017015111 scopus 로고
    • Estimating fatigue crack lives for aircraft techniques
    • (1976) Exp. Mech , vol.16 , Issue.11 , pp. 425-433
    • Gallagher, J.P.1
  • 26
    • 34250605357 scopus 로고
    • Fatigue: A complex subject-some simple approximation
    • (1965) Exp. Mech , vol.5 , pp. 193-202
    • Manson, S.S.1
  • 29
    • 0002294908 scopus 로고
    • Analysis of an infinite plate containing radial cracks originating at the boundary of an internal circular hole
    • (1956) J. Math. Phys , vol.25 , pp. 60-71
    • Bowie, O.L.1


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.