In Chapter 2 the fatigue life until failure has been divided into two periods: (i) the crack initiation period, and (ii) crack growth period. Crack nucleation and microcrack growth in the first period are primarily phenomena occurring at the material surface. The second period starts when the fatigue crack penetrates into the subsurface material away from the material surface. The growth of the fatigue crack is then depending of the crack growth resistance of the material as a bulk property. The two previous chapters, Chapters 6 and 7, mainly deal with fatigue in the crack initiation period. The subject of the present chapter is fatigue crack growth in the second period. It could also be referred to as the growth of macro fatigue cracks.
Under which conditions is crack growth in the second period of practical interest? Obviously, the load spectrum should contain stress cycles above the fatigue limit in order to have a fatigue crack problem. Secondly, some macrocrack growth must be acceptable, but it should then be known how fast crack growth occurs. Two well-known examples are:
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(i)
Crack growth in sheet material where the crack is growing through the full thickness of the material. An obvious example is fatigue crack growth in aircraft skin structures.
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(ii)
A second example is the growth of part through cracks, see Figure 5.3 where a corner crack or a surface crack starts at a hole. Part through cracks also occur as surface cracks in welded structures at the toe of a weld. In many practical cases, part through cracks are associated with massive components and thick plate structures.
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References
Standard test method for measurement of fatigue crack growth rates. ASTM Standard E64791 (1991).
Paris, P.C., Gomez, M.P. and Anderson, W.E., A rational analytical theory of fatigue. The Trend of Engineering, Vol. 13 (1961), pp. 9–14.
Schijve, J., Fatigue crack propagation and the stress intensity factor. Faculty of Aerospace Engineering, Delft, Memorandum M-191 (1973).
Figge, I.E. and Newman, Jr, J.C., Fatigue-crack-propagation behavior in panels with simulated rivet forces. NASA TN D-4702 (1968).
Schijve, J., Significance of fatigue cracks in micro-range and macro-range. ASTM-STP 415, (1967) pp. 415–459.
Wanhill, R.J.H., Durability analysis using short and long fatigue crak growth data. Aircraft Damage Assessment and Repair. The Institution of Engineering, Australia (1991). Barton, Australia.
Paris, P.C. and Erdogan, F., A critical analysis of crack propagation laws. Trans. ASME, Series D, Vol. 85 (1963), pp. 528–535.
Forman, R.G., Kearney, V.E. and Engle, R.M., Numerical analysis of crack propagation in cyclic-loaded structures. J. Basic Engrg., Trans. ASME, Vol. D89 (1967), pp. 459–464.
Priddle, E.K., High cycle fatigue crack propagation under random and constant amplitude loadings. Int. J. Pressure Vessels & Piping, Vol. 4 (1976), p. 89.
Klesnil, M. and Lukáš, P., Influence of strength and stress history on growth and stabilization of fatigue cracks. Engrg. Fracture Mech., Vol. 4 (1972), pp. 77–92.
Elber, W., The significance of fatigue crack closure. Damage tolerance in aircraft structures. ASTM STP 486 (1971), pp. 230–242.
Rice, J.R., The mechanics of crack tip deformation and extension by fatigue. Fatigue crack propagation. ASTM STP 415 (1967), pp. 247–309.
Schijve, J., Some formulas for the crack opening stress level. Engrg. Fracture Mechanics, Vol. 14 (1981), pp. 461–465.
Van der Linden, H.H., NLR test results as a database to be used in a check of crack propagation prediction models. A Garteur activity. Nat. Aerospace Lab. NLR, TR 79121U, Amsterdam (1979).
Schijve, J., Fatigue crack closure observations and technical significance. Mechanics of Fatigue Crack Closure, Int. Symp., Charleston 1986. ASTM STP 982 (1988), pp. 5–34.
Ewalds, H.L. and Furnee, R.T., Crack closure measurements along the crack front in center cracked specimens. Int. J. Fracture, Vol. 14 (1978), pp. R53–R55.
Sunder, R. and Dash, P.K., Measurement of fatigue crack closure through electron microscopy. Int. J. Fatigue, Vol. 4 (1982), pp. 97–105.
Ritchie, R.O., Mechanisms of fatigue crack propagation in metals, ceramics and composites: Role of crack tip shielding. Mater. Sci. Engrg., Vol. A103 (1988), pp. 15–28.
Broek, D. and Schijve, J., The influence of the mean stress on the propagation of fatigue cracks in aluminium alloy sheet. Nat. Aerospace Lab. NLR, Report TR M.2111, Amsterdam (1963).
Crooker, T.W., The role of fracture toughness in low-cycle fatigue crack propagation for high-strength alloys. Engrg. Fracture Mech., Vol. 5 (1973), pp. 35–43.
Stephens, R.R., Stephens, R.I., Veit, A.L. and Albertson, T.P., Fatigue crack growth of Ti-62222 alloy under constant amplitude and mini-TWIST flight spectra at 25°C and 175°C. Int. J. Fatigue, Vol. 19 (1997), pp. 301–308.
Houdijk, P.A., Effect of specimen thickness and specimen geometry on fatigue crack growth in Fe510Nb. Faculty of Chemistry and Materials, Delft University of Technology (1993) [in Dutch].
Song-Hee Kim and Weon-Pil Tai, Retardation and arrest of fatigue crack growth in AISI 4340 steel by introducing rest periods and overloads. Fatigue Fracture Engrg. Mater. Structure, Vol. 15 (1992), pp. 519–530.
Liaw, P.K., Peck, M.G. and Rudd, G.E., Fatigue crack growth behavior of D6AC space shuttle steel. Engrg. Fracture Mech., Vol. 43 (1992), pp. 379–400.
Newman, J.C., Jr. and Raju, I.S., Stress-intensity factor equation for crack in three-dimensional finite bodies subjected to tension and bending loads. Fracture Mechanics, ASTM STP 791, Vol. 1 (1983), pp. 238–265.
Petrak, G.S., Strength level effects on fatigue crack growth and retardation. Engrg. Fracture Mech., Vol. 6 (1974), pp. 725–733.
Schijve, J. and De Rijk, P., The fatigue crack propagation in 2024-T3 Alclad sheet materials from seven different manufacturers. Nat. Aerospace Lab. NLR, Report TR M.2162, Amsterdam (1966).
Yoder, G.R., Cooley, L.A. and Crooker, T.W., The effect of load ratio on fatigue crack growth in Ti-8Al-1Mo-1V. Engrg. Fracture Mech., Vol. 17 (1983), pp. 185–188.
Kage, M., Miller, K.J. and Smith, R.A., Fatigue crack initiation and propagation in a low-carbon steel of two different grain sizes. Fatigue Fracture Engrg. Mater. Structure, Vol. 15 (1992), pp. 763–774.
Wanhill, R.J.H., Low stress intensity fatigue crack growth in 2024-T3 and T351. Engr. Fracture Mech., Vol. 30 (1988), pp. 233–260.
Stubbington, C.A. and Gunn, N.J.F., Effects of fatigue crack front geometry and crystallography on the fracture toughness of an Ti-6Al-4V alloy. Roy. Aero. Est., TR 77158, Farnborough (1977).
Pearson, S., Initiation of fatigue cracks in commercial aluminium alloys and the subsequent propagation of very short cracks. Engrg. Fracture Mech., Vol. 7 (1975), pp. 235–247.
Schijve, J. and Hoeymakers, A.H.W., Fatigue crack growth in lugs and the stress intensity factor. Fatigue Engrg. Mater. Structures, Vol. 1 (1979), pp. 185–201.
Poe, Jr., C.C., Fatigue crack propagation in stiffened panels. Damage tolerance in aircraft structures, ASTM STP 486 (1971), pp. 79–97.
Ichsan, S. Putra and Schijve, J., Crack opening stress measurements of surface cracks in 7075-T6 Al alloy plate specimens through electron fractography. Fatigue Fracture. Engrg. Mater. Structures, Vol. 15 (1992), pp. 323–338.
Lin, X.B. and Smith, R.A., Fatigue shape analysis for corner cracks at fastener holes. Engrg. Fracture Mech., Vol. 59 (1998), pp. 73–87.
Broek, D., The Practical Use of Fracture Mechanics. Kluwer Academic Publishers (1988).
Fawaz, S.A., Fatigue Crack Growth in Riveted Joints. Doctor Thesis, Delft University of Technology (1997).
Fawaz, S.A. and Andersson, B., Accurate stress intensity factor solutions for corner cracks at a hole. Engrg. Fracture Mech., Vol. 71 (2004), pp. 1235–1254.
Newman, J.C., Jr. and Raju, I.S., Stress-intensity factor equation for crack in three-dimensional finite bodies subjected to tension and bending loads. Fracture Mechanics, ASTM STP 791, Vol. 1 (1983), pp. 238–265.
Harter, J.A., AFGROW Users Guide and Technical Manual, AFGROW version 4.0012.15, AFRL-VA-WP-TR-2007 (2007).
Wang, S.-H. and Müller, C., A study on the change of fatigue fracture mode in two titanium alloys. Fatigue Fracture Engrg. Mater. Structure, Vol. 21 (1998), pp. 1077–1087.
De Freitas, M. and Francois, D., Analysis of fatigue crack growth in rotary bend specimens and railway axles. Fatigue Fracture Engrg. Mater. Structure, Vol. 18 (1995), pp. 171–178.
Carpinteri, A., Handbook of Fatigue Crack Propagation in Metallic Structures. Elsevier, Amsterdam (1994).
Blom, A.F. and Beevers, C.J. (Eds.), Theoretical Concepts and Numerical Analysis of Fatigue. Proc. Conf. May 1992, Birmingham. EMAS (1992).
Anderson, T.L., Fracture Mechanics: Fundamentals and Applications. CRC Press (1991).
Reuter, W., Underwood, J.H. and Newman, Jr., J.C. (Eds.), Surface-crack growth: Models, experiments, and structures. ASTM STP 1060 (1990).
Brown, M.W. and Miller, K.J. (Eds.), Biaxial and Multiaxial Fatigue. EGF Publication 3. Mechanical Engineering Publications (1989).
Newman, Jr., J.C. and Elber, W. (Eds.), Mechanics of Fatigue Crack Closure. ASTM STP 982 (1988).
Miller, K.J. and Brown, M.W. (Eds.), Multiaxial Fatigue. ASTM STP 853 (1985).
Pook, L.P., The Role of Crack Growth in Metal Fatigue. The Metals Society, London (1983).
ESDU Engineering Science Data. Fatigue-Fracture Mechanics Data. Vol. 2 (aluminium alloys) and Vol. 3 (Titanium alloys and steels). (1981–1999).
Fatigue Crack Propagation, ASTM STP 415 (1967).
Hudson, C.M. and Seward, S.K., A compendium of sources of fracture toughness and fatigue crack growth data for metallic alloys. Parts I, II and III. Int. J. Fracture, Vol. 14 (1978) pp. R151–R184, Vol. 20 (1982) pp. R59–R117, Vol. 39 (1989) pp. R43–R63.
McClung, R.C., The influence of applied stress, crack length, and stress intensity factor on crack closure. Metallurgical Trans., Vol. 22a (1991), pp. 1559–1571.
Wanhill, R.J.H., Microstructural influences on fatigue and fracture resistance in high strength structural materials. Engrg. Fracture Mech., Vol. 10 (1978), pp. 337–357.
Short Crack Growth Behaviour in Various Aircraft Materials, AGARD Report No. 767 (1990).
Schijve, J., Difference between the growth of small and large fatigue cracks. The relation to threshold K-values. Fatigue Thresholds, Fundamentals and Engineering Applications. Proc. Int. Conf. Stockholm 1981. EMAS Warley (1982), pp. 881–908.
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(2009). Fatigue Crack Growth. Analysis and Predictions. In: Schijve, J. (eds) Fatigue of Structures and Materials. Springer, Dordrecht. https://doi.org/10.1007/978-1-4020-6808-9_8
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