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fatigue crack growth rate

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Published: 01 December 2000
Fig. 12.31 Effect of heat treatment on fatigue crack growth rate in Ti-6Al-4V alloy. L-T, longitudinal-transverse More
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Published: 01 December 2000
Fig. 12.32 Effect of welding processes on fatigue crack growth rate of longitudinally oriented titanium alloys. (a) Ti-6Al-4V alpha-beta alloy. (b) Ti-15V-3Cr-3Al-3Sn beta alloy. GTAW, gas-tungsten arc welding; EBW, electron beam welding; LBW, laser beam welding More
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Published: 01 August 2005
Fig. 3.17 Schematic illustration of variation of fatigue crack growth rate, da/dN , with alternating stress intensity, Δ K , in steels, showing regions of primary crack growth mechanisms More
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Published: 01 August 2005
Fig. 5.38 Fatigue crack growth rate correlation technique More
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Published: 01 August 2005
Fig. 5.42 Typical shape of a fatigue crack growth rate curve for a given R value More
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Published: 01 August 2005
Fig. 5.43 Fatigue crack growth rate data for 2024-T351 aluminum with six R -ratios More
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Published: 01 August 2005
Fig. 5.51 Effect of stress ratio on fatigue crack growth rate threshold for several aluminum alloys. Source: Ref 5.27 More
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Published: 01 August 2005
Fig. 5.52 Effect of stress ratio on fatigue crack growth rate threshold for titanium alloys. Source: Ref 5.54 More
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Published: 01 August 2005
Fig. 5.53 Effect of stress ratio on fatigue crack growth rate threshold for several low- to medium-strength steels. Source: Ref 5.55 More
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Published: 01 December 2004
Fig. 8.26 Fatigue crack growth rate ( R = 0.1) versus stress-intensity factor at room temperature for A356.0-T6 aluminum alloy castings produced by various processes More
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Published: 01 December 2004
Fig. 8.27 Fatigue crack growth rate ( R = 0.5) versus stress-intensity factor at room temperature for A356.0-T6 aluminum alloy castings produced by various processes More
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Published: 01 July 2000
Fig. 7.120 Corrosion-fatigue-crack-growth rate as a function of stress-intensity range for a maraging steel in air and 3% NaCl solution. Source: Ref 171 More
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Published: 01 July 2000
Fig. 7.121 Corrosion-fatigue-crack-growth rate as a function of stress-intensity range for high-strength 4340M steel in vacuum and distilled water at 23 °C. Data for vacuum and indicated frequencies and R = 0. Source: Ref 172 More
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Published: 01 July 2000
Fig. 7.122 Corrosion-fatigue-crack-growth rate as a function of stress-intensity range for X-65 line pipe steel in air and in 3.5% NaCl solution under cathodic coupling to zinc. Cycled at indicated frequencies and R = 0.2. Coupled potential = –800 ± 10 mV (SHE). (Note: Original reference More
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Published: 01 July 2000
Fig. 7.123 Corrosion-fatigue-crack-growth rate as a function of stress-intensity range for X-65 line pipe steel in air and at the free corrosion potential in 3.5% NaCl at indicated frequencies and R = 0.2. Corrosion potential = –440 ± 30 mV (SHE). (Note: Original reference includes data More
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Published: 01 July 2000
Fig. 7.124 Corrosion-fatigue-crack-growth rate as a function of stress-intensity range for Ti-6Al-4V alloy in air and in 0.6 M NaCl at indicated frequencies and R = 0.1. Source: Ref 170 More
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Published: 01 July 2000
Fig. 7.125 Corrosion-fatigue-crack-growth rate as a function of stress-intensity range for a high-strength aluminum alloy in dry argon and indicated halide solutions. Source: Ref 173 More
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Published: 01 July 2009
Fig. 17.40 Fatigue crack growth rate versus K Ic for vacuum hot-pressed S-65 and S-200E. Source: Lemon and Brown 1985 More
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Published: 01 July 2009
Fig. 17.41 Fatigue crack growth rate for experimental grade C beryllium as a function of maximum applied stress-intensity factor, K fmx , at the crack tip for a range of specimen thicknesses. Solid line b is theoretical. Source: Auten and Hanafee 1976 More
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Published: 01 March 2002
Fig. 12.38 Fatigue crack growth rate behavior of IN-718 nickel-base superalloy tested in air at 649 °C (1200 °F) More