Prediction of fatigue crack growth under constant amplitude loading and a single overload based on elasto-plastic crack tip stresses and strains

Engineering Fracture Mechanics

Volumn 75, Issue 2, 2008, Pages 188-206

  Noroozi, A H ^a   Glinka, G ^a   Lambert, S ^a  

^a UNIVERSITY OF WATERLOO   (Canada)

Author keywords

Driving force; Fatigue crack growth; Single overload; Stress ratio; Two parameter driving force

Indexed keywords

ALUMINUM ALLOYS; COMPUTER SIMULATION; CRACK TIPS; CYCLIC LOADS; ELASTOPLASTICITY; FATIGUE DAMAGE; RESIDUAL STRESSES; STRAIN RATE; STRESS INTENSITY FACTORS;

DRIVING FORCE; MEAN STRESS; REVERSED CYCLIC PLASTICITY;

FATIGUE CRACK PROPAGATION;

ALUMINUM ALLOYS; COMPUTER SIMULATION; CRACK TIPS; CYCLIC LOADS; ELASTOPLASTICITY; FATIGUE CRACK PROPAGATION; FATIGUE DAMAGE; RESIDUAL STRESSES; STRAIN RATE; STRESS INTENSITY FACTORS;

EID: 36048975692     PISSN: 00137944     EISSN: None     Source Type: Journal    
DOI: 10.1016/j.engfracmech.2007.03.024     Document Type: Article

References (38)

1. Paris P.C., and Erdogan F. A critical analysis of crack propagation laws. J Basic Engng D85 (1963) 528-534
2. Elber W. The significance of fatigue crack closure. In: Damage tolerance in aircraft structure, ASTM STP 486. American Society for Testing and Materials; 1971. p. 230-42.
3. Macha D.E., Corby D.M., and Jones J.W. On the variation of fatigue-crack-opening load with measurement location. Exp Mech 19 6 (1979) 207-213
4. Shih T.T., and Wei R.P. A study of crack closure in fatigue. Engng Fract Mech 6 1 (1974) 19-32
5. 0.5 driving force parameter for crack growth in aluminum alloys. Int J Fatigue 23 8 (2001) 733-740
6. eff estimation procedure on 6061-T6 and 2024-T3 aluminum alloys. Int J Fatigue 21 S1 (1999) 47-57
7. Kirby B.R., and Beevers C.J. Slow fatigue crack growth and threshold behavior in air and vacuum of commercial aluminum alloys. Fatigue Engng Mater Struct 1 2 (1979) 203-215
8. Walker EK. The effect of stress ratio during crack propagation and fatigue for 2024-T3 and 7075-T6 aluminum. In: Effect of environment and complex load history on fatigue life, ASTM STP 462, American Society for Testing and Materials; 1970. p. 1-14.
9. Vasudevan A.K., Sadananda K., and Louat N. A review of crack closure, fatigue crack threshold and related phenomena. Mater Sci Engng A188 1-2 (1994) 1-22
10. + parameters. Engng Fract Mech 71 12 (2004) 1779-1790
11. Wheeler O.E. Spectrum loading and crack growth. Trans ASME, J Basic Engng 94 1 (1972) 181-186
12. Willenborg J, Engle RM, Wood HA. A crack growth retardation model using an effective stress concept. Report No. AFFDL TM-71-1- FBR, USAF. Air Force Flight Dynamic Laboratory; 1971.
13. De Koning AU. A simple crack closure model for prediction of fatigue crack growth rates under variable-amplitude loading. In: Roberts R, editor. Fract Mech, ASTM STP 743. American Society for Testing and Materials; 1981. p. 63-85.
14. Padmadinata UH. Investigation of crack-closure prediction models for fatigue in aluminum alloy sheet under flight-simulation loading. Report LR-619. Delft University of Technology, Faculty of Aerospace Engineering; 1990.
15. Newman JR. Prediction of fatigue crack growth under variable-amplitude and spectrum loading using a closure model. In: Abelkis PR, Hudson CM, editors. Design of fatigue and fracture resistant structure, ASTM STP 761. American Society for Testing and Materials; 1982. p. 255-77.
16. McEvily A.J., and Yang Z. In: Czoboly E. (Ed). Failure analysis - theory and practice (1988), Engineering Materials Advisory Services, Warley, UK 1231-1248
17. Noroozi A.H., Glinka G., and Lambert S. A two parameter driving force for fatigue crack growth analysis. Int J Fatigue 27 10-12 (2005) 1277-1296
18. Bowles CQ. The role of environment, frequency, and shape during fatigue crack growth in aluminum alloys. Doctoral Dissertation. Delft University, The Netherlands; 1978.
19. Jones R. Private communications. DSTO Centre for Structural Mechanics, Department of Mechanical Engineering, Monash University, Victoria, Australia; 2006.
20. Pommier S. A study of the relationship between variable level fatigue crack growth and the cyclic constitutive behavior of steel. Int J Fatigue 23 S1 (2001) 111-118
21. Sander M., and Richard H.A. Lifetime prediction for real loading situations-concepts and experimental results of fatigue crack growth. Int J Fatigue 25 9-11 (2003) 999-1005
22. Ramberg W, Osgood WR. Description of stress-strain curves by three parameters. NACA Technical Note No. 902. Notational Advisory Committee for Aeronautics; 1943.
23. Tavernelli J.F., and Coffin L.F. Experimental support for generalized equation predicting low cycle fatigue, and Manson SS. Discussion. Trans ASME, J Basic Engng 84 4 (1962) 533-541
24. Smith K.N., Watson P., and Topper T.H. A stress-strain function for the fatigue of metals. J Mater 5 4 (1970) 767-778
25. Creager M., and Paris P.C. Elastic field equations for blunt cracks with reference to stress corrosion cracking. Int J Fract Mech 3 4 (1967) 247-252
26. Neuber H. Theory of stress concentration for shear-strained prismatic bodies with arbitrary nonlinear stress-strain law. Trans ASME, J Appl Mech 28 (1961) 544-551
27. Molski K., and Glinka G. A method of elastic-plastic stress and strain calculation at a notch root. Mat Sci Engng 50 1 (1981) 93-100
28. Glinka G., ott W., and Nowack H. Elastoplastic plane strain analysis of stresses and strains at the notch root. J Engng Mater Technol Trans ASME 110 3 (1988) 195-204
29. Glinka G. Relations between the strain energy density distribution and elastic-plastic stress-strain fields near cracks and notches and fatigue life calculation. In: Slomon HD, Halford GR, Kaisand LR, Leis BN, editors. Low cycle fatigue, ASTM STP 942. American Society for Testing and Materials; 1988. p. 1022-47.
30. Glinka G, Buczynski A. In: Kalluri S et al. editors. Multi-axial fatigue and deformation, ASTM STP 1387. American Society for Testing and Materials; 2000. p. 82-98.
31. Skrzypek J.J., and Hetnarski R.B. Plasticity and creep: theory, examples and problems (1993), CRC Press, Boca Raton
32. Shen G., and Glinka G. Determination of weight functions from reference stress intensity factor. Theor Appl Fract Mech 15 3 (1991) 237-245
33. Wang X., Lambert S., and Glinka G. Approximate weight functions for embedded elliptical cracks. Engng Fract Mech 59 3 (1998) 381-392
34. Jiang Y. Private communications. Department of Mechanical Engineering, University of Nevada, Reno; 2005.
35. Dubensky RG. Fatigue crack propagation in 2024-T3 and 7075-T6 aluminum alloys at high stress. Report No. NASA CR-1732; 1971.
36. Hudson CM. Effect of stress ratio on fatigue crack growth in 7075-T6 and 2024-T3 aluminum alloy specimens. Report No. NASA TN D-5390; 1969.
37. Newman JC, Wu X R, Venneri SL, Li CG. Small-crack effects in high strength aluminum alloys - A NASA/CAE cooperative program. NASA Reference Publication 1309; 1994.
38. Chanani G.R. Retardation of fatigue-crack growth in 7075 aluminum. Met Engng Quart 5 1 (1975) 40-48