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Volumn 19, Issue 8, 1996, Pages 997-1008

Equivalent constant amplitude concepts examined under fatigue crack propagation by block loading

Author keywords

Aluminium alloy 2024 T35; Crack closure; Energy dissipation; Equivalent constant amplitude loading; Fatigue crack propagation; Variable amplitude loading

Indexed keywords

CRACK PROPAGATION; ENERGY DISSIPATION; FATIGUE OF MATERIALS; FATIGUE TESTING; LOADS (FORCES);

EID: 0030206835     PISSN: 8756758X     EISSN: None     Source Type: Journal    
DOI: 10.1111/j.1460-2695.1996.tb01035.x     Document Type: Article
Times cited : (14)

References (15)
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  • 5
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    • ASTM STP 486, American Society for Testing and Materials, Philadelphia
    • W. Elber (1971) The significance of fatigue crack closure, ASTM STP 486, pp. 230-241. American Society for Testing and Materials, Philadelphia.
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  • 7
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    • Energy required for fatigue crack propagation
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    • N. Ranganathan, J. Petit and J. de Fouquet (1987) Energy required for fatigue crack propagation. In: Strength of Metals and Alloys (Edited by H. J. McQueen, J. P. Bailon, J. I. Dickson, J. J. Jonas and M. J. Akben), Vol. 2, pp. 1267-1272. Pergamon Press, Oxford, UK.
    • (1987) Strength of Metals and Alloys , vol.2 , pp. 1267-1272
    • Ranganathan, N.1    Petit, J.2    De Fouquet, J.3
  • 8
    • 0343562808 scopus 로고
    • A fatigue crack propagation study under flight simulation loading based on a reduced spectrum
    • (Edited by J. Petit, P. Rabbe, S. Suresh and D. Davidson) Elsevier Applied Science Publishers, London
    • M. Benguediab, N. Ranganathan, J. Petit, M. R. Cazus, B. Lachaud and J. M. Thomas (1988) A fatigue crack propagation study under flight simulation loading based on a reduced spectrum. In: Fatigue Crack Propagation Under Variable Amplitude Loading (Edited by J. Petit, P. Rabbe, S. Suresh and D. Davidson), pp. 309-325. Elsevier Applied Science Publishers, London.
    • (1988) Fatigue Crack Propagation under Variable Amplitude Loading , pp. 309-325
    • Benguediab, M.1    Ranganathan, N.2    Petit, J.3    Cazus, M.R.4    Lachaud, B.5    Thomas, J.M.6
  • 9
    • 0023850551 scopus 로고
    • Low stress intensity fatigue crack growth in 2024T3 and T351
    • R. J. H. Wanhill (1988) Low stress intensity fatigue crack growth in 2024T3 and T351. Engng Fract. Mech. 30(2), 223-260.
    • (1988) Engng Fract. Mech. , vol.30 , Issue.2 , pp. 223-260
    • Wanhill, R.J.H.1
  • 10
    • 0023531710 scopus 로고
    • Crack propagation studies in Al7475 on the basis of constant amplitude and selected variable amplitude loading histories
    • S. Zhang, R. Marissen, K. Schulte, K. K. Trautmann, H. Novack and J. Schijve (1987) Crack propagation studies in Al7475 on the basis of constant amplitude and selected variable amplitude loading histories. Fatigue Fract. Engng Mater. Struct. 10(2), 315-332.
    • (1987) Fatigue Fract. Engng Mater. Struct. , vol.10 , Issue.2 , pp. 315-332
    • Zhang, S.1    Marissen, R.2    Schulte, K.3    Trautmann, K.K.4    Novack, H.5    Schijve, J.6
  • 12
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    • Some formulas for the crack opening level
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    • Schijve, J.1
  • 13
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    • Damage evaluation of metals for random loading - Three aspects of the rainflow method
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  • 14
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    • Current status of flight simulation fatigue crack growth concepts
    • (Edited by J. Petit, P. Rabbe, S. Suresh and D. Davidson) Elsevier Applied Science Publishers, London
    • R. J. H. Wanhill and J. Schijve (1988) Current status of flight simulation fatigue crack growth concepts. In: Fatigue Crack Propagation Under Variable Amplitude Loading (Edited by J. Petit, P. Rabbe, S. Suresh and D. Davidson), pp. 309-325. Elsevier Applied Science Publishers, London.
    • (1988) Fatigue Crack Propagation under Variable Amplitude Loading , pp. 309-325
    • Wanhill, R.J.H.1    Schijve, J.2


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.