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Published: 01 January 1996
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Published: 01 January 2000
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(a) Fatigue crack propagation regimes and (b) crack growth rates of wrought...
Available to PurchasePublished: 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
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Book Chapter
Fatigue Crack Growth Markers to Aid Quantitative Fractography
Available to PurchaseBook: Fractography
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...
Abstract
This article discusses several examples of fatigue load histories that intentionally create artificial fracture-surface markings during testing such that they are measurable by post-test quantitative fractography (QF). It reviews a number of methods for providing fatigue fracture-surface markers to aid QF of fatigue crack growth (FCG). These methods are based on load changes, including reordering the basic load histories and/or adding loads to them. The article also provides some guidelines for obtaining recognizable FCG markers for a variety of load histories and crack-growth regimes for coupons, components, and, particularly, full-scale fatigue tests.
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Published: 01 January 1997
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Schematic representation of fatigue crack growth curve (stress intensity ve...
Available to PurchasePublished: 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
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Illustration of the three distinct regimes of crack propagation rate observ...
Available to PurchasePublished: 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
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Image
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
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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
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in Service Lifetime Assessment of Polymeric Products
> Characterization and Failure Analysis of Plastics
Published: 15 May 2022
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Effect of orientation on stage II (Paris regime) fatigue crack-growth rate ...
Available to PurchasePublished: 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
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Crack-growth rate curve for stress-corrosion cracking. (a) Idealized crack ...
Available to PurchasePublished: 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
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Book: Fatigue and Fracture
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...
Abstract
The approaches to spectrum life prediction in components can be classified into two types, namely, history-based methods, using the life-fraction rule or other damage rules, and postservice evaluation methods. This article discusses the variables affecting the material crack growth rate behavior and those essential elements in making spectrum crack growth life prediction. It provides information on life assessment for bulk creep damage.
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Crack growth rate curve for stress-corrosion cracking. (a) Idealized crack ...
Available to PurchasePublished: 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
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Book Chapter
Microstructure-Sensitive Modeling and Simulation of Fatigue
Available to PurchaseSeries: 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...
Abstract
The purposes and methods of fatigue modeling and simulation in high-cycle fatigue (HCF) regime are to design either failsafe components or components with a finite life and to quantify remaining life of components with pre-existing cracks using fracture mechanics, with the intent of monitoring via an inspection scheme. This article begins with a discussion on the stages of the fatigue damage process. It describes hierarchical multistage fatigue modeling and several key points regarding the physics of crack nucleation and microstructurally small crack propagation in the HCF regime. The article provides a description of the microstructure-sensitive modeling to model fatigue of several classes of advanced engineering alloys. It describes the various modeling and design processes designed against fatigue crack initiation. The article concludes with a discussion on the challenges in microstructure-sensitive fatigue modeling.
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Schematic representation of fatigue crack propagation behavior. In regime I...
Available to PurchasePublished: 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
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Image
Schematic representation of fatigue crack propagation behavior. In regime I...
Available to PurchasePublished: 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
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Heuristic multistage modeling framework for nucleation and growth of fatigu...
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in Microstructure-Sensitive Modeling and Simulation of Fatigue
> Fundamentals of Modeling for Metals Processing
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
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Book Chapter
Behavior of Small Fatigue Cracks
Available to PurchaseBook: Fatigue and Fracture
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...
Abstract
This article defines different types of small cracks and identifies the different factors that influence small-crack behavior. Appropriate analysis techniques, including both rigorous scientific and practical engineering treatments, are briefly described. Important material data issues are addressed, including increased scatter in small-crack data and recommended small-crack test methods. The article highlights the applications where small cracks may be particularly important.
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Schematic fatigue crack-growth curve showing the three stages of long crack...
Available to PurchasePublished: 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
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