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Book Chapter
Nonarbitrary Crack Size Concept for Fatigue Crack Initiation
Available to PurchaseSeries: ASM Technical Books
Publisher: ASM International
Published: 01 August 2005
DOI: 10.31399/asm.tb.mmfi.t69540379
EISBN: 978-1-62708-309-6
... Abstract This appendix presents an analytical model that estimates damage rates for both crack initiation and propagation mechanisms. The model provides a nonarbitrary definition of fatigue crack initiation length, which serves as an analytical link between initiation and propagation analyses...
Abstract
This appendix presents an analytical model that estimates damage rates for both crack initiation and propagation mechanisms. The model provides a nonarbitrary definition of fatigue crack initiation length, which serves as an analytical link between initiation and propagation analyses and appears to have considerable merit in estimating the total fatigue life of notched and cracked structures.
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Influence of texture on fatigue crack growth in Ti-6Al-4V. Fatigue crack gr...
Available to Purchase
in Fatigue and Fracture of Engineering Alloys
> Fatigue and Fracture<subtitle>Understanding the Basics</subtitle>
Published: 01 November 2012
Fig. 58 Influence of texture on fatigue crack growth in Ti-6Al-4V. Fatigue crack growth rates are higher when basal planes are loaded in tension. The elastic modulus in tension for the basal texture (B) is 109 GPa (15.8 × 10 6 psi); for the transverse texture (T), 126 GPa (18.3 × 10 6 psi
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Fatigue crack growth behavior of 7075-T6 aluminum under remote and crack-li...
Available to PurchasePublished: 01 August 2005
Fig. 5.40 Fatigue crack growth behavior of 7075-T6 aluminum under remote and crack-line loading conditions. Source: Ref 5.41
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Fatigue crack growth testing and data analysis. (a) Crack length measuremen...
Available to PurchasePublished: 30 June 2023
Fig. 9.16 Fatigue crack growth testing and data analysis. (a) Crack length measurement, (b) calculation of crack growth rate, and (c) analysis of da/dN versus stress intensity range.
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Fatigue crack growth per fatigue cycle ( da / dN ) versus stress intensity ...
Available to PurchasePublished: 01 October 2011
Fig. 7.25 Fatigue crack growth per fatigue cycle ( da / dN ) versus stress intensity variation ( Δ K ) per cycle. The C and n are constants that can be obtained from the intercept and slope, respectively, of the linear log da / dN versus log Δ K plot. This equation for fatigue crack
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Fatigue failure surface from a piston rod. The fatigue crack initiated near...
Available to PurchasePublished: 01 October 2011
Fig. 16.24 Fatigue failure surface from a piston rod. The fatigue crack initiated near a forging flake at the center and propagated slowly outward. The outer area is the region of final brittle fracture overload. Source: Ref 16.5
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Thermal fatigue failure and conventional fatigue crack propagation fracture...
Available to PurchasePublished: 01 December 2003
Fig. 3 Thermal fatigue failure and conventional fatigue crack propagation fracture during reversed load cycling of acetal. Source: Ref 10
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Thermal fatigue crack produced in the hardfacing alloy on an exhaust valve ...
Available to PurchasePublished: 01 October 2011
Fig. 16.13 Thermal fatigue crack produced in the hardfacing alloy on an exhaust valve from a heavy-duty gasoline engine
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Scanning electron micrograph of fatigue crack initiating on worn carbonitri...
Available to Purchase
in Mechanisms and Causes of Failures in Heat Treated Steel Parts
> Failure Analysis of Heat Treated Steel Components
Published: 01 September 2008
Fig. 15 Scanning electron micrograph of fatigue crack initiating on worn carbonitrided steel. Original magnification: approximately 4000×
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Published: 01 September 2008
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Published: 01 September 2008
Fig. 18 Schematic representation of the R ratio effect on fatigue crack growth curves. The near-threshold, Paris regime, and final failure regions are also indicated on the curves.
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Fatigue crack site. (a) General view. (b) Detail. The inclusion that origin...
Available to PurchasePublished: 01 September 2008
Fig. 31 Fatigue crack site. (a) General view. (b) Detail. The inclusion that originated the site was removed from the fracture surface. SEM image with secondary electrons
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Concentration of inclusions near the fatigue crack site. (a) SEM image with...
Available to PurchasePublished: 01 September 2008
Fig. 32 Concentration of inclusions near the fatigue crack site. (a) SEM image with secondary electrons. (b) Backscattered electrons
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Model of fatigue crack initiation due to the presence of inclusions in a no...
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in Sources of Failures in Carburized and Carbonitrided Components
> Failure Analysis of Heat Treated Steel Components
Published: 01 September 2008
Fig. 70 Model of fatigue crack initiation due to the presence of inclusions in a nonmartensitic (decarburized) steel layer. Source: Ref 122
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Location of fatigue crack initiation on nitrided 40HM (4140)-grade steel. O...
Available to PurchasePublished: 01 September 2008
Fig. 9 Location of fatigue crack initiation on nitrided 40HM (4140)-grade steel. Original magnification: 100×
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Surface fracture spring. The dotted arrow shows the fatigue crack nucleus, ...
Available to Purchase
in Steel Failures due to Tempering and Isothermal Heat Treatment
> Failure Analysis of Heat Treated Steel Components
Published: 01 September 2008
Fig. 27 Surface fracture spring. The dotted arrow shows the fatigue crack nucleus, and the dashed arrow shows the fatigue-to-brittle fracture transition. The solid arrow shows the surface analyzed by scanning electron microscopy. Original magnification: 6×
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Specimens employed in fatigue crack propagation studies. (a) Single-edge-no...
Available to PurchasePublished: 01 December 2003
Fig. 7 Specimens employed in fatigue crack propagation studies. (a) Single-edge-notch specimen. (b) Compact-tension specimen
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Comparison of fatigue crack propagation behavior in the Paris regime for se...
Available to PurchasePublished: 01 December 2003
Fig. 11 Comparison of fatigue crack propagation behavior in the Paris regime for several amorphous and semicrystalline polymers. Note enhanced fatigue resistance of the semicrystalline polymers. PC, polycarbonate; PMMA, polymethyl methacrylate; PPO, polypropylene oxide; PVF, polyvinyl formal
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Fatigue crack propagation behavior for a rubber-toughened epoxy. The additi...
Available to PurchasePublished: 01 December 2003
Fig. 12 Fatigue crack propagation behavior for a rubber-toughened epoxy. The addition of rubber decreases the slope, m , at high crack growth rates due to toughening mechanisms and retarded crack growth. CTBN, carboxylterminated polybutadiene acrylonitrile rubber; MBS, methacrylate-butadiene
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Published: 01 December 2003
Fig. 8 An S-shaped fatigue crack propagation. K , stress-intensity factor; K c , fracture toughness curve indicating its three characteristic regions.
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