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stress failure

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Published: 01 July 2000
Fig. 7.91 Sustained tensile-stress failure time for 76 mm (3 in.) plate of 7075-T651 aluminum alloy. Shaded bands indicate combinations of stress and time known to produce SCC in specimens intermittently immersed in 3.5% NaCl solution. Point A is the minimum yield strength in the long transverse More
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Published: 01 November 2010
Fig. 17.37 Peel stress failure of thick composite joints. Source: after Ref 12 More
Series: ASM Technical Books
Publisher: ASM International
Published: 01 January 2017
DOI: 10.31399/asm.tb.sccmpe2.t55090419
EISBN: 978-1-62708-266-2
...Abstract Abstract This chapter describes nondestructive evaluation (NDE) test methods and their relative effectiveness for diagnosing the cause of stress-corrosion cracking (SCC) service failures. It discusses procedures for analyzing various types of damage in carbon and low-alloy steels, high...
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Published: 01 March 2006
Fig. A.59 Probability of failure as a function of stress amplitude for a failure to occur before a specified number of cycles More
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Published: 01 November 2012
Fig. 17 (a) Stress versus log cycles to failure curve. (b) Log stress versus log cycles to failure curve. Source: Ref 11 More
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Published: 01 January 2017
Fig. 11.6 Effect of temperature on time to failure of stress split rings (stress = 310 MPa, or 45 ksi) of Zircaloy-2 with an iodine content, I 2 , of 3 × 10 −3 g/cm 2 . Source: Ref 11.18 More
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Published: 01 November 2012
Fig. 18 Stress versus log cycles to failure curves for bending and axial loading tests of 4340 steel. Source: Ref 11 More
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Published: 01 November 2012
Fig. 19 Log true stress versus log reversals to failure of 4340 steel. From Fatigue Design Handbook , SAE. Source: Ref 11 More
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Published: 01 November 2012
Fig. 18 Intergranular failure in nickel-base alloy. Inconel 751, stress rupture at 1350 °F, 55 ksi, 125 h. Source: Ref 8 More
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Published: 01 October 2012
Fig. 10.14 Stress amplitude-failure cycles ( S - N ) plot of 3 mol%-yttria-stabilized zirconia tensile specimens for various R -ratios. Solid lines show CARES/LIFE predictions at 50% reliability using the Walker slow crack growth law to predict strength degradation due to cyclic fatigue. Source More
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Published: 01 February 2005
Fig. 22.20 Tensile maximum principal stress in failure area [ Hannan et al., 2001 ] More
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Published: 01 January 2000
Fig. 53 Stress-corrosion failure of an Apollo Ti-6Al-4V RCS pressure vessel due to nitrogen tetroxide. (a) Failed vessel after exposure to pressurized N 2 O 4 for 34 h. (b) Cross section through typical stress-corrosion cracks. 250× More
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Published: 01 January 2000
Fig. 54 Stress-corrosion failure of a type 304 stainless steel heat exchanger tube from carbon dioxide compressor intercooler after exposure to a pressurized chloride-containing (200 ppm) environment at 120 °C (250 °F) (a) Cracks on the external surface. (b) Cracks originating on the external More
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Published: 01 December 2000
Fig. 12.16 Curves depicting stress versus cycles to failure for pure titanium as affected by (a) grain size, (b) oxygen content, and (c) cold work More
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Published: 01 December 2000
Fig. 12.17 Curves depicting room-temperature stress versus cycles to failure for grade 2 titanium (0.03 wt% iron) at two temperatures. UTS, ultimate tensile strength More
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Published: 01 December 2000
Fig. 12.18 Curves depicting room-temperature stress versus cycles to failure for alpha-beta titanium alloy Ti-6Al-4V in a variety of conditions. (a) Fully lamellar structure. (b) Fully equiaxed structure. (c) Duplex microstructure. In (a), width of alpha lamellae is at issue; in (b), effect More
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Published: 01 December 2000
Fig. 12.20 Curves depicting stress versus cycles to failure (R = –1) for Ti-1100 near-alpha titanium alloy. (a) Full lamellar microstructures showing range of effects of prior-beta grain sizes. (b) Duplex microstructures showing range of effects of primary alpha content More
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Published: 01 December 2000
Fig. 12.25 Curves depicting stress versus cycles to failure for various microstructures in Ti-10V-2Fe-3Al beta alloy for various levels of primary alpha. R = –1. More
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Published: 01 December 2000
Fig. 12.27 Curves depicting stress versus cycles to failure for coarse-grained Ti-8Al alpha alloy with and without thermomechanical processing to produce local grain refinement at the surface More
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Published: 01 December 2000
Fig. 12.28 Curves depicting stress versus cycles to failure for Ti-6Al-2Sn-4Zr-2Mo alloy with and without thermomechanical processing to produce local grain refinement at the surface More