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Volumn 23, Issue 7, 2000, Pages 603-617

Model for fatigue crack growth, Part II: Modelling

Author keywords

[No Author keywords available]

Indexed keywords

ALUMINUM ALLOYS; COMPRESSIVE STRESS; CRACK PROPAGATION; CYCLIC LOADS; FATIGUE OF MATERIALS; MATHEMATICAL MODELS; RESIDUAL STRESSES; STRESS INTENSITY FACTORS; TENSILE STRESS; YIELD STRESS;

EID: 0034430350     PISSN: 8756758X     EISSN: None     Source Type: Journal    
DOI: 10.1046/j.1460-2695.2000.00298.x     Document Type: Article
Times cited : (25)

References (16)
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  • 3
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  • 5
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    • (1977) ICF4 , vol.2 , pp. 1353-1360
    • Pellas, J.1    Baudin, G.2    Roberts, M.3
  • 6
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    • Crack growth model for flight-type loading
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    • Baudin, G.1    Robert, M.2
  • 7
    • 0018291433 scopus 로고
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    • Broek, D.1    Smith, S.H.2
  • 8
    • 0019686176 scopus 로고
    • A simple crack closure model for prediction of fatigue crack growth rates under variable amplitude loading
    • American Society for Testing and Materials, West Conshohocken, PA, USA
    • A. U. De Koning (1980) A simple crack closure model for prediction of fatigue crack growth rates under variable amplitude loading. In: ASTM STP 743. American Society for Testing and Materials, West Conshohocken, PA, USA, pp. 63-85.
    • (1980) ASTM STP 743 , pp. 63-85
    • De Koning, A.U.1
  • 9
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  • 10
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    • (1987) ASTM STP 982 , pp. 491-504
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  • 11
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* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.