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fatigue crack growth
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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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Published: 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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Published: 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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Published: 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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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)
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Published: 01 March 2002
Fig. 12.39 Schematic of idealized fatigue crack growth curve. R , minimum stress divided by maximum stress in a fatigue cyce
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Published: 01 March 2002
Fig. 12.41 Effect of grain size on fatigue crack growth rate of AP-1 nickel-base superalloy at room temperature
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Published: 01 March 2002
Fig. 12.42 Effect of grain size on fatigue crack growth rate of P/M Astroloy at 649 °C (1200 °F)
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Published: 01 March 2002
Fig. 12.45 Effect of air vs. helium on fatigue crack growth rate of IN-718 nickel-base superalloy at 649 °C (1200 °F)
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Published: 01 June 1983
Figure 8.13 Schematic plot of fatigue crack growth rate data trends, illustrating the sigmoidal curve of da / dN vs. Δ K .
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Published: 01 June 1983
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Published: 01 June 1983
Figure 8.15 Fatigue crack growth rate data for an Fe–21Cr–6Ni–9Mn steel, illustrating stress ratio effects at two test temperatures.
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Published: 01 June 1983
Figure 8.16 Effect of temperature on the fatigue crack growth rates of AISI 310S, an f.c.c. alloy.
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Published: 01 June 1983
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Published: 01 June 1983
Figure 8.18 Effect of temperature on the fatigue crack growth rates of Fe-9Ni steel, a b.c.c. alloy.
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Published: 01 June 1983
Figure 8.19 Effect of temperature on the fatigue crack growth rates of Ti-5AI-2.5Sn, an h.c.p. alloy.
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Published: 01 June 1983
Figure 11.9 Fatigue crack growth rates of AISI type 304L austenitic stainless steel at 295, 76, and 4 K ( Tobler and Reed, 1978 ).
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Published: 01 June 1983
Figure 11.17 Fatigue crack growth rates at 4 K of an 18Cr–10Ni austenitic stainless steel with variable carbon plus nitrogen interstitial contents ( Tobler and Reed, 1982 ). 1 —0.067% C+N; 2 — 0.097% C+N; 3 — 0.128% C+N; 4–9 — 0.157–0.325% C+N.
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Published: 01 June 1983
Figure 11.34 Fatigue crack growth rates for 9% Ni steel at 4, 76, 111, and 295 K ( Tobler et al., 1975 ).
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Published: 01 November 2012
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