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Volumn 23, Issue SUPPL. 1, 2001, Pages

Model prediction of fatigue crack propagation in metal alloys in laboratory air

Author keywords

Fatigue crack propagation; Fracture mechanics; Metals; Process zone; Published experimental data

Indexed keywords

CRACK PROPAGATION; ELASTIC MODULI; FRACTURE MECHANICS; FRACTURE TOUGHNESS; STRESS INTENSITY FACTORS;

EID: 0035207032     PISSN: 01421123     EISSN: None     Source Type: Journal    
DOI: 10.1016/s0142-1123(01)00138-4     Document Type: Article
Times cited : (14)

References (37)
  • 6
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    • A crack-closure model for predicting fatigue under aircraft spectrum loading
    • (1981) ASTM STP , vol.748 , pp. 53-85
    • Newman J.C., Jr.1
  • 15
    • 0015457452 scopus 로고
    • Threshold for fatigue crack propagation and effects of load ratio and frequency
    • Progress in Flaw Growth and Fracture Toughness Testing
    • (1973) ASTM STP , vol.536 , pp. 79-94
    • Schmidt, R.A.1    Paris, P.C.2
  • 20
    • 85167867406 scopus 로고
    • Mean stress and environmental effects on near threshold fatigue crack growth, cracks and fracture
    • (1976) ASTM STP , vol.601 , pp. 154-168
    • Mautz, J.1    Weiss, V.2
  • 25
    • 84986346923 scopus 로고
    • Effect of R factor and crack closure on fatigue crack growth in aluminum and titanium alloys
    • (1974) ASTM STP , vol.559 , pp. 264-282
    • Katcher, M.1    Kaplan, M.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.