Overloads in ductile and brittle materials

Fatigue and Fracture of Engineering Materials and Structures

Volumn 28, Issue 11, 2005, Pages 971-981

  Pippan, R ^a,b   Bichler, C ^a,c   Tabernig, B ^a,d   Weinhandl, H ^a  

^a ERICH SCHMID INSTITUTE OF MATERIALS SCIENCE   (Austria)

^b INSTITUTE FOR MICROELECTRONICS   (Austria)

^c AUSTRIAN INSTITUTE OF TECHNOLOGY   (Austria)

^d PLANSEE SE   (Austria)

Author keywords

Crack closure; Fatigue crack propagation; Periodic overloads; Single overload; Threshold

Indexed keywords

ALUMINUM ALLOYS; BRITTLENESS; DUCTILITY; HARDENING; STEEL; STRAIN;

CRACK CLOSURE; FATIGUE CRACK PROPAGATION; PERIODIC OVERLOADS; SINGLE OVERLOAD; THRESHOLD;

CRACK PROPAGATION;

EID: 28044455419     PISSN: 8756758X     EISSN: 14602695     Source Type: Journal    
DOI: 10.1111/j.1460-2695.2005.00934.x     Document Type: Article

References (28)

1. Schijve, J. (1960) Fatigue crack propagation in light alloy sheet material and structures. In: NRL Report MP National Aeronautical Research Institute, Amsterdam, Holland, 195.
2. Elber, W (1971) Significance of fatigue crack closure. Damage tolerance in aircraft structures. ASTM STP 486, American Society for Testing and Materials, pp. 230-242.
3. Von Euw, E. F. J., Hertzberg, R. W. and Roberts, R. (1973) Stress analyses and growth of cracks. ASTM STP 513, American Society for Testing and Materials, pp. 230-259.
4. Christensen, R. H. (1959) Metal fatigue, McGraw-Hill, New York.
5. Hudson, C. M. and Hardrath, H.F. (1961) Effects of changing stress amplitude on the rate of fatigue crack propagation of two aluminium alloys. NASA Technical Note National Aeronautics and Space Administration, Washington, DC, D-960.
6. Suresh, S. (1983) Micromechanisms of fatigue crack growth retardation following overloads. Engng Fract. Mech. 18, 577-593.
7. Jones, R. E. (1973) Fatigue crack growth retardation after single cycle peak overload in Ti-6Al-4V titanium alloy. Engng Fract. Mech. 5, 585-604.
8. Knott, J. F. and Pickard, A.C. (1977) Effects of overloads on fatigue crack propagation: aluminum alloys. Engng Fract. Mech. Metal Science 11, 399-304.
9. Forsyth, P. J. E. (1984) In: Fatigue 84, (Edited by C.J. Beevers) EMAS Ltd., Warley U.K. 2:637.
10. Lang, M. (2000) A model for fatigue crack growth, Part I: Phenomenology and Part II: Modelling. Fatigue Fract. Engng Mater. Struct. 23, 587-617.
11. Schijve, J. (1979) Four lectures on fatigue crack growth. Engng Fract. Mech. 11, 167-221.
12. Bichler, C. and Pippan, R. (1999) Direct observation of the residual plastic deformation caused by a single overload. In: Advances in fatigue crack closure measurement and analysis. Vol. 2, ASTM STP 1342 (Edited by R.C. McChung and J. C. Newman Jr.). West Conshohocken, PA: American Society for Testing and Materials, pp. 191-206.
13. Skorupa, M. (1999) Load interaction effects during fatigue crack growth under variable amplitude loading-a literature review. Part ii: Qualitative interpretation. Fatigue Fract. Engng Mater. Struct. 22, 905-926.
14. Bichler, C. (1999) Rissspiteenverformung bei konstanter und variabler Belastungs-amplitude. Motatanuniversität Leoben, thesis.
15. Bichler, C. (1995) Vergleich der zyklischen Rissspitzenverformung und des Riss-schliessens zwischen Oberfläche und Probenmitte. Montanuniversität Leoben, diploma thesis.
16. Bao, H. and McEvily, A. J. (1998) On plane stress-plane strain interaction in fatigue crack growth, Int. J. Fatigue 20, 441-448.
17. Siegmund, T., Kolednik, O. and Pippan, R. (1990) Direkte Messung der Rissspitzen-verformung bei wechselnder Belastung. Z. Metallkunde 81, 677-689.
18. Sommitsch, C. (1995) Bestimmung del- zyklischen Rissö ffnungsverschiebung und der Rissschließkraft beim Ermü dungsfortschritt. Montanuniversität Leoben, diploma thesis.
19. Tomkins, B. and Biggs, W. D. (1969) Low endurance fatigue in metals and polymers. J. Mater. Sci. 4, 544-553.
20. McClung, R. C. (1991) The influence of applied stress, crack length, and stress intensity factor on crack closure. Met. Trans. A. 22, 1559-1571.
21. Newman, J. C., Jr. (1999) Prediction of crack growth under variable-amplitude loading in thin-steel 2024-T3 aluminum alloys. In: Engineering against fatigue, (Edited by J. H. Beynon, M. W. Brown, R. A. Smith, T. C. Lindley and B. Tomkins). A. A. Balkema, Rotterdam, pp. 261-263.
22. Tabernig, B. (2000) Ermüdungsverhalten teilchenverstärkter Aluminiumlegierungen. Montanuniversität Leohen, thesis.
23. Tabernig, B., Pippan, R., Foulquier, Rapaport, A. and Sereni, S. (2003) Periodic overloads in the near threshold regime. Astm Stp, in press, doi: 10.1520/JAI19061.
24. Pelloux, R. M. N. (1996) Mechanisms of formation of ductile fatigue striations. Trans. ASM, 62, 281-285.
25. Bichler, C. and Pippan, R. (1999) Direct observation of the formation of striations. In: Engineering against fatigue (Edited by J.H. Beynon, M. W Brown, T.C. Lindley, R. A. Smith and B. Tomkins). A.A. Balkema, Rotterdam, pp. 211-218.
26. Bruzsii, M. (2000) Development models to predict the mechanical response of aluminium and aluminium matrix composites in static and fatigue loading. National University of Ireland, Galway, thesis.
27. 3 particle-reinforced 6061 aluminum alloy. Fatigue Fract. Engng Mater. Struct. 18, 477-487.
28. Tabernig, B. and Pippan, R. (2004) Effect of periodic overloads in particle-reinforced aluminum alloys: the near threshold behavior. Int. J. Fatigue 26, 323-330.