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fatigue properties

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Published: 30 June 2023
Fig. 9.15 Flexural fatigue properties ( R = 0) of aluminum alloy beams produced from wrought and cast aluminum alloys. Source: Ref 9.11 More
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Published: 01 June 2008
Fig. 28.13 Effect of hot isostatic pressing (HIP) on fatigue properties of Ti-6Al-4V investment castings. Room temperature smooth bar, tension-tension fatigue, R = +0.1 Source: Ref 2 More
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Published: 01 October 2011
Fig. 10.24 Effect of cast section size on the fatigue properties of pearlitic and ferritic ductile irons More
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Published: 01 March 2002
Fig. 12.84 Comparison of fatigue properties of SCDS MAR-M-200, with carbide sizes ranging from “large carbides” to “moderate” (a) to “carbide-free” (b) More
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Published: 01 November 2012
Fig. 54 Effect of hot isostatic pressing (HIP) on fatigue properties of Ti-6Al-4V investment castings. Room-temperature smooth bar, tension-tension fatigue, R = +0.1. Source: Ref 35 More
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Published: 01 November 2012
Fig. 11 Fatigue properties of aerospace materials. Source: Ref 1 More
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Published: 01 March 2006
Fig. 11.6 Axial fatigue properties of SAE 4340 steel (unidirectional and reversed loading) as a function of material cleanliness for L 50 life. Source: Ref 11.10 More
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Published: 01 March 2006
Fig. 11.35 Effect of surface conditions on fatigue properties of nickel-base alloy Inconel 718, cantilever bending, zero mean stress, 24 °C (75 °F). Source: Ref 11.41 More
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Published: 01 March 2006
Fig. 11.43 Effect of environment on axial tensile fatigue properties of S-816 at 816 °C (1500 °F) in both vacuum and air. Source: Ref 11.46 More
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Published: 01 October 2012
Fig. 5.34 Effect of hot isostatic pressing (HIP) on fatigue properties of Ti-6Al-4V investment castings. Room-temperature smooth bar; tension-tension fatigue; R = +0.1. Source: Ref 5.4 More
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Published: 01 October 2012
Fig. 8.1 Fatigue properties of aerospace materials. Source: Ref 8.1 More
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Published: 01 December 1989
Fig. 4.8. S-N curves for IN-738 LC ( Ref 4 ). High-cycle fatigue properties of extrafine-grain and conventional material tested at 850 °C (1560 °F), showing the effect of grain size. More
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Published: 01 December 1989
Fig. 9.47. Scatterband for low-cycle-fatigue properties at 850 °C (1560 °F) for IN 738 LC tested at two different frequencies ( Ref 75 ). More
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Published: 01 November 2010
Fig. 14.11 Fatigue properties of aerospace materials. Source: Ref 13 More
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Published: 01 November 2010
Fig. 1.20 Fatigue properties of aerospace materials More
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Published: 01 December 2004
Fig. 8.4 Flexural fatigue properties ( R = 0) of aluminum alloy beams produced from wrought and cast aluminum alloys. Source: Ref 20 More
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Published: 01 December 2004
Fig. 8.5 Fatigue properties of 295.0 aluminum alloy castings with various degrees of porosity. Source: Ref 22 More
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Published: 01 December 2004
Fig. 8.6 Fatigue properties of conventionally cast and squeeze cast aluminum alloy A356.0-T6. Source: Ref 23 More
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Published: 01 December 2004
Fig. 8.7 Rotating beam ( R = –1.0) fatigue properties of notched specimens from wrought and cast aluminum alloys. Source: Ref 21 More
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Published: 01 December 2004
Fig. 8.8 Axial-stress ( R = 0) fatigue properties of welded aluminum alloy castings. Source: Ref 21 More