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Volumn 29, Issue 8, 2007, Pages 1393-1401

The influence of mean stress on fatigue crack propagation in aluminium alloys

Author keywords

Crack propagation; Fatigue; Mean stress; Stress ratio

Indexed keywords

ALUMINUM ALLOYS; DATA REDUCTION; NUMERICAL METHODS; STRESS ANALYSIS;

EID: 33947690780     PISSN: 01421123     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.ijfatigue.2006.11.010     Document Type: Article
Times cited : (36)

References (21)
  • 1
    • 0015055746 scopus 로고    scopus 로고
    • Elber W. The significance of fatigue crack closure. In: Damage tolerance in aircraft structures. ASTM STP 486, Philadelphia, 1971. p. 230-42. ISBN 0-8031-0072-8.
  • 2
    • 33947690658 scopus 로고    scopus 로고
    • Walker K. The effect of stress ratio during crack propagation and fatigue for 2024-T3 and 7075-T6 aluminum. In: Effects of environment and complex load history on fatigue life. ASTM STP 462, Philadelphia, 1970. p. 1-14. ISBN 8031-0050-7.
  • 3
    • 0035452427 scopus 로고    scopus 로고
    • 0.5 driving force parameter for crack growth in aluminium alloys
    • 0142-1123
    • 0.5 driving force parameter for crack growth in aluminium alloys. Int J Fatigue, 0142-1123 23 (2001) 733-740
    • (2001) Int J Fatigue , vol.23 , pp. 733-740
    • Kujawski, D.1
  • 4
    • 0242493470 scopus 로고    scopus 로고
    • Parametric study on the variability of opening load determination
    • 0142-1123
    • Kujawski D., and Stoychev S. Parametric study on the variability of opening load determination. Int J Fatigue, 0142-1123 25 (2003) 1181-1187
    • (2003) Int J Fatigue , vol.25 , pp. 1181-1187
    • Kujawski, D.1    Stoychev, S.2
  • 5
    • 27144447064 scopus 로고    scopus 로고
    • eff and their implications on FCG predictions
    • 0142-1123
    • eff and their implications on FCG predictions. Int J Fatigue, 0142-1123 27 (2005) 1267-1276
    • (2005) Int J Fatigue , vol.27 , pp. 1267-1276
    • Kujawski, D.1
  • 6
    • 0019398428 scopus 로고
    • Some formulas for the crack opening stress level
    • 0013-7944
    • Schijve J. Some formulas for the crack opening stress level. Eng Fract Mech, 0013-7944 14 3 (1981) 461-465
    • (1981) Eng Fract Mech , vol.14 , Issue.3 , pp. 461-465
    • Schijve, J.1
  • 7
    • 33947625514 scopus 로고    scopus 로고
    • Mann T. Fatigue assessment methods for welded structures and their application to an aluminium T-joint. PhD thesis, Norwegian University of Science and Technology, Trondheim, 2006. ISBN 82-471-8020-0.
  • 8
    • 0035300869 scopus 로고    scopus 로고
    • Fatigue crack growth and crack closure in an AlMgSi alloy
    • 1460-2695
    • Borrego L.P., Ferreira J.M., and Costa J.M. Fatigue crack growth and crack closure in an AlMgSi alloy. Fatigue Fract Eng Mater Struct, 1460-2695 24 4 (2001) 255-265
    • (2001) Fatigue Fract Eng Mater Struct , vol.24 , Issue.4 , pp. 255-265
    • Borrego, L.P.1    Ferreira, J.M.2    Costa, J.M.3
  • 9
    • 0040891375 scopus 로고
    • The influence of the mean stress on the propagation of fatigue cracks in aluminium alloy sheet
    • Broek D., and Schijve J. The influence of the mean stress on the propagation of fatigue cracks in aluminium alloy sheet. NLR-TR M2111 (1963)
    • (1963) NLR-TR M2111
    • Broek, D.1    Schijve, J.2
  • 10
    • 0022525762 scopus 로고
    • Comparison of short and long fatigue crack growth in 7075-T6 aluminum
    • 8756-758X
    • Bu R., and Stephens R.I. Comparison of short and long fatigue crack growth in 7075-T6 aluminum. Fatigue Fract Eng Mater Struct, 8756-758X 9 1 (1986) 35-48
    • (1986) Fatigue Fract Eng Mater Struct , vol.9 , Issue.1 , pp. 35-48
    • Bu, R.1    Stephens, R.I.2
  • 11
    • 0033227627 scopus 로고    scopus 로고
    • eff estimation procedures on 6061-T6 and 2024-T3 aluminum alloys
    • 0142-1123
    • eff estimation procedures on 6061-T6 and 2024-T3 aluminum alloys. Int J Fatigue, 0142-1123 21 Suppl. 1 (1999) S47-S57
    • (1999) Int J Fatigue , vol.21 , Issue.SUPPL. 1
    • Donald, K.1    Paris, P.C.2
  • 13
    • 22544463528 scopus 로고
    • Metals and Cheramics Information Center, Battelle
    • MCIC. Damage tolerant design handbook (1972), Metals and Cheramics Information Center, Battelle
    • (1972) Damage tolerant design handbook
    • MCIC1
  • 14
    • 0037306514 scopus 로고    scopus 로고
    • Fatigue crack propagation prediction by cyclic plasticity damage accumulation models
    • 8756-758X
    • Durán J.A.R., Castro J.T.P., and Filho J.C.P. Fatigue crack propagation prediction by cyclic plasticity damage accumulation models. Fatigue Fract Eng Mater Struct, 8756-758X 26 2 (2003) 137-150
    • (2003) Fatigue Fract Eng Mater Struct , vol.26 , Issue.2 , pp. 137-150
    • Durán, J.A.R.1    Castro, J.T.P.2    Filho, J.C.P.3
  • 17
    • 33947643055 scopus 로고    scopus 로고
    • Hudson CM. Effect of stress ratio on fatigue-crack growth in 7075-T6 and 2024-T3 aluminum-alloy specimens. NASA TN D-5390, 1969.
  • 18
    • 33645987918 scopus 로고    scopus 로고
    • Fatigue crack growth analysis of welded aluminium RHS T-joints with manipulated residual stress level
    • 8756-758X
    • Mann T., Tveiten B.W., and Härkegård G. Fatigue crack growth analysis of welded aluminium RHS T-joints with manipulated residual stress level. Fatigue Fract Eng Mater Struct, 8756-758X 29 2 (2006) 113-122
    • (2006) Fatigue Fract Eng Mater Struct , vol.29 , Issue.2 , pp. 113-122
    • Mann, T.1    Tveiten, B.W.2    Härkegård, G.3
  • 19
    • 0032201845 scopus 로고    scopus 로고
    • Small crack growth and fatigue life predictions for high-strength aluminium alloys: Part I - Experimental and fracture mechanics analysis
    • 8756-758X
    • Wu X.R., Newman J.C., Zhao W., Swain M.H., Ding C.F., and Phillips E.P. Small crack growth and fatigue life predictions for high-strength aluminium alloys: Part I - Experimental and fracture mechanics analysis. Fatigue Fract Eng Mater Struct, 8756-758X 21 11 (1998) 1289-1306
    • (1998) Fatigue Fract Eng Mater Struct , vol.21 , Issue.11 , pp. 1289-1306
    • Wu, X.R.1    Newman, J.C.2    Zhao, W.3    Swain, M.H.4    Ding, C.F.5    Phillips, E.P.6
  • 20
    • 0019627111 scopus 로고    scopus 로고
    • Newman Jr JR. A crack closure model for predicting fatigue crack growth under aircraft spectrum loading. In: Methods and models for predicting fatigue crack growth under random loading. ASTM STP 748, Philadelphia, 1981. p. 53-84.


* 이 정보는 Elsevier사의 SCOPUS DB에서 KISTI가 분석하여 추출한 것입니다.