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X-ray diffraction stress versus applied stress for varying average roughnes...
Available to Purchase
in X-Ray Diffraction Residual Stress Measurement in Failure Analysis
> Failure Analysis and Prevention
Published: 01 January 2002
Fig. 6 X-ray diffraction stress versus applied stress for varying average roughness ( R a ). (a) Samples with R a of 1, 3, and 6 μm. (b) Samples with R a of 1, 40, and 56 μm. (Source: Ref 26 )
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in X-Ray Diffraction Residual Stress Measurement in Failure Analysis
> Failure Analysis and Prevention
Published: 01 January 2002
Image
X-ray diffraction stress versus applied stress on (a) as-received and (b) e...
Available to Purchase
in X-Ray Diffraction Residual Stress Measurement in Failure Analysis
> Failure Analysis and Prevention
Published: 01 January 2002
Fig. 9 X-ray diffraction stress versus applied stress on (a) as-received and (b) electropolished surfaces
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in Corrosion Fatigue and Stress-Corrosion Cracking in Metallic Biomaterials
> Corrosion: Environments and Industries
Published: 01 January 2006
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X-ray diffraction (XRD) stress versus applied stress for varying average ro...
Available to Purchase
in X-Ray Diffraction Residual-Stress Measurement in Failure Analysis
> Failure Analysis and Prevention
Published: 15 January 2021
Fig. 6 X-ray diffraction (XRD) stress versus applied stress for varying average roughness ( R a ). (a) Samples with R a of 1, 3, and 6 μm. (b) Samples with R a of 1, 40, and 56 μm. Source: Ref 35
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Ratio of measured stress (XRD, x-ray diffraction) and applied stress for va...
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in X-Ray Diffraction Residual-Stress Measurement in Failure Analysis
> Failure Analysis and Prevention
Published: 15 January 2021
Fig. 7 Ratio of measured stress (XRD, x-ray diffraction) and applied stress for varying average roughness, R a . Source: Ref 35
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Image
X-ray diffraction stress versus applied stress on (a) as-received and (b) e...
Available to Purchase
in X-Ray Diffraction Residual-Stress Measurement in Failure Analysis
> Failure Analysis and Prevention
Published: 15 January 2021
Fig. 9 X-ray diffraction stress versus applied stress on (a) as-received and (b) electropolished surfaces
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Image
Published: 01 January 1990
Fig. 22 J c normalized to zero applied stress as a function of stress, σ, at indicated fields for Cu-Nb-Sn, Cu-V-Ga in situ composites, and a conventional commercial V 3 Ga composite. Source: Ref 34
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Published: 01 January 1996
Fig. 14 Crack-tip stress intensity ( K I ) in terms of applied stress (σ) for (a) a center-cracked plate and (b) an edge-cracked plate under uniform tension
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Published: 01 January 1996
Fig. 4 Crack-tip stress-intensity ( K I ) in terms of applied stress (σ) for (a) a center-cracked plate and (b) an edge-cracked plate under uniform tension. The crack shown in (a) is defined as 2 a and the crack shown in (b) is defined as a, because of the convention that any crack
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in Corrosion Fatigue and Stress-Corrosion Cracking in Metallic Biomaterials[1]
> Materials for Medical Devices
Published: 01 June 2012
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Published: 01 January 2002
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Published: 01 January 2002
Fig. 12 Critical crack depth vs. applied stress for WF14 × 730 H-section, a/c = 0.5, δ m = 0.25 mm (0.010 in.)
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Variant coalescence of 18R martensite in Cu-Zn-Ga under applied stress. Sou...
Available to PurchasePublished: 01 December 2004
Fig. 42 Variant coalescence of 18R martensite in Cu-Zn-Ga under applied stress. Source: Ref 42 . Reprinted with permission
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Schematic diagram of time to failure versus applied stress, σ, normalized t...
Available to PurchasePublished: 01 January 2003
Fig. 28 Schematic diagram of time to failure versus applied stress, σ, normalized to the yield strength σ y for stress corrosion
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Relationship of applied stress and flaw depth to crack propagation in hydro...
Available to PurchasePublished: 01 January 2003
Fig. 60 Relationship of applied stress and flaw depth to crack propagation in hydrogen gas. Dashed lines show an example of the use of such a chart for a steel with K th of 60.5 MPa m (55 ksi in . at an operating stress of 359 MPa (52 ksi). Source: Ref 159
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Hydrogen embrittlement crack growth rate as a function of applied stress in...
Available to PurchasePublished: 01 January 2003
Fig. 7 Hydrogen embrittlement crack growth rate as a function of applied stress intensity for two different hardnesses and environments for an AISI 4340 steel, contoured double-cantilever beam test specimen
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Response of a four-parameter model to a constant applied stress, where σ 0 ...
Available to PurchasePublished: 01 November 1995
Fig. 12 Response of a four-parameter model to a constant applied stress, where σ 0 is the applied stress and t 0 is the removal time of the applied stress. The solid line represents the four-parameter response; the dotted line, the Voigt-Kelvin element response; the dashed line
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Applied stress versus life of tensile-type stainless steel specimens in sim...
Available to PurchasePublished: 01 December 1998
Fig. 11 Applied stress versus life of tensile-type stainless steel specimens in simulated sea water
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Hydrogen embrittlement crack growth rate as a function of applied stress in...
Available to PurchasePublished: 01 December 1998
Fig. 14 Hydrogen embrittlement crack growth rate as a function of applied stress intensity for two different hardnesses and environments for an AISI 4340 steel contoured double-cantilever beam test specimen
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