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Volumn 25, Issue 8-9, 2002, Pages 727-733

Near threshold fatigue crack growth versus long finite life

Author keywords

Fatigue crack growth; Fatigue cracking threshold; Giga cycle fatigue; Load displacement characteristics; Partial closure model

Indexed keywords

ALUMINUM ALLOYS; CRACK INITIATION; CRACK PROPAGATION; CYCLIC LOADS; ELASTIC MODULI; STRESS INTENSITY FACTORS;

EID: 0036674074     PISSN: 8756758X     EISSN: None     Source Type: Journal    
DOI: 10.1046/j.1460-2695.2002.00560.x     Document Type: Article
Times cited : (10)

References (11)
  • 3
    • 0005390047 scopus 로고
    • The rate of fatigue crack growth in two aluminum alloys
    • NASA-Technical Note no. 4394
    • (1958)
    • McEvilly, A.J.1    Illg, W.2
  • 5
    • 0005390048 scopus 로고
    • Extremely slow fatigue crack growth rates in aluminum alloy 7075-T6
    • MSc Thesis (directed by Prof. P. Paris), Lehigh University
    • (1965)
    • Linder, B.M.1
  • 7
    • 0002106959 scopus 로고
    • Threshold for fatigue crack growth and the effects of load ratio and frequency
    • ASTM-STP 536
    • (1973)
    • Schmidt, R.A.1    Paris, P.C.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.