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Published: 01 January 1996
Fig. 2 Fatigue crack growth regimes versus Δ K More
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Published: 01 January 2000
Fig. 2 Fatigue crack growth regimes versus Δ K More
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Published: 15 June 2019
Fig. 39 (a) Fatigue crack propagation regimes and (b) crack growth rates of wrought aluminum alloys. L-T, longitudinal transverse; T-L, transverse longitudinal. Source: Ref 65 More
Series: ASM Handbook
Volume: 12
Publisher: ASM International
Published: 01 June 2024
DOI: 10.31399/asm.hb.v12.a0006877
EISBN: 978-1-62708-387-4
... regimes for coupons, components, and, particularly, full-scale fatigue tests. crack-growth regimes fatigue crack growth markers fatigue test quantitative fractography DURING DESIGN and when considering the in-service structural integrity of mechanical systems, some testing is usually done...
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Published: 01 January 1997
Fig. 10 Schematic illustrating three different regimes of crack growth More
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Published: 15 June 2020
Fig. 12 Schematic representation of fatigue crack growth curve (stress intensity versus crack velocity) showing three primary crack growth regimes: (I) crack initiation, (II) stable crack growth (Paris regime), and (III) unstable/critical crack growth leading to fracture More
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Published: 15 May 2022
Fig. 7 Illustration of the three distinct regimes of crack propagation rate observed in fatigue testing under constant amplitude loading conditions. The first region is denoted by the dashed line to the left. This is the threshold and near-threshold growth region. Crack driving forces must More
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Published: 01 January 1996
Fig. 50 Fatigue crack growth of 7075 and 2024 plate in moist air, R = 0.33 (a) 25 vs 200 Hz with crack growth regimes (b) and (c) typical scatterbands More
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Published: 15 June 2019
Fig. 40 Fatigue crack growth of 7075 and 2024 plate in moist air, R = 0.33. (a) 25 vs. 200 Hz with crack growth regimes. (b) Typical scatter bands for two alloys. L-T, longitudinal transverse More
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Published: 15 May 2022
Fig. 14 Application of Paris’ law to Regime B brittle fatigue crack growth data More
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Published: 01 June 2024
Fig. 17 Effect of orientation on stage II (Paris regime) fatigue crack-growth rate using the Paris law parameters measured on strongly textured Ti-6Al-4V sheet. The orientations represent (hkil) || cracking plane and [uvtw] || crack-growth direction. Courtesy of Dr. M.C. Brandes. Source: Ref More
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Published: 01 December 1998
Fig. 12 Crack-growth rate curve for stress-corrosion cracking. (a) Idealized crack growth rate curve where regime I is SCC enhancement of cracking above the threshold. In regime II, mechanical enhancement has attained a maximum, and cracking is transport controlled. In regime III, the process More
Book Chapter

By A.F. Liu
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002390
EISBN: 978-1-62708-193-1
... be characterized in terms of fracture mechanic crack growth by the steady-state (large-scale crack growth regime) parameter C ∗ and the transient parameter C t . The parameter C t is theoretically equivalent to K (the crack-tip stress-intensity factor) under small-scale creep. It becomes C ∗ when...
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Published: 01 January 1996
Fig. 12 Crack growth rate curve for stress-corrosion cracking. (a) Idealized crack growth rate curve where regime I is SCC enhancement of cracking above the threshold. In regime II the mechanical enhancement has attained a maximum and cracking is transport controlled. In regime III the process More
Series: ASM Handbook
Volume: 22A
Publisher: ASM International
Published: 01 December 2009
DOI: 10.31399/asm.hb.v22a.a0005405
EISBN: 978-1-62708-196-2
... at the end of the initiation process, a i , is based either on consistency with crack lengths measured in smooth specimens to define the strain-life relations, typically 0.5 to 1 mm, or some nonarbitrary length corresponding to a transition from a regime of growth that is affected by the notch root stress...
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Published: 01 December 1998
Fig. 10 Schematic representation of fatigue crack propagation behavior. In regime I, the crack-growth rate is low because the threshold for crack propagation is approached. In regime II, the Paris law is obeyed, while in regime III, the crack-growth rate increases above that predicted More
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Published: 01 January 1996
Fig. 10 Schematic representation of fatigue crack propagation behavior. In regime I the crack growth rate is low since the threshold for crack propagation is approached. In regime II the so-called Paris law is obeyed while in regime III the crack growth rate increases above that predicted More
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Published: 01 December 2009
Fig. 3 Heuristic multistage modeling framework for nucleation and growth of fatigue cracks. Cycles N MSC and N PSC , respectively, represent the number of cycles to propagate the crack(s) in the regimes of microstructurally small crack (MSC) growth (normally 3–10 times the grain or second More
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002358
EISBN: 978-1-62708-193-1
..., and the statistically averaged material properties become smoother. However, it is important to note that the fundamental mechanism of crack growth is often the same for small and large cracks in the near-threshold regime. In both cases, FCG occurs as an intermittent process involving strain range accumulation...
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Published: 01 June 2024
Fig. 16 Schematic fatigue crack-growth curve showing the three stages of long crack growth and the small-crack regime where there is strong microstructural influence that leads to accelerated crack-growth rates. Adapted from Ref 40 More