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endurance
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Published: 01 December 1989
Fig. 4.5. Influence of environment on fatigue endurance of 2¼Cr-1Mo steel in sodium, air, and helium at 865 K ( Ref 4 ). The cycle used was approximately up for 5 s, hold for 5 s, down for 5 s, hold for 5 s.
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Published: 01 December 1989
Fig. 4.14. Effects of hold time and tensile vs compressive hold on cyclic endurance life of 1Cr-Mo-V rotor steel at 565 °C (1050 °F) ( Ref 29 ).
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Published: 01 December 1989
Fig. 4.15. Types of LCF cycles employed, and corresponding endurance data, for a 1Cr-Mo-V rotor steel ( Ref 34 ). (a) Type II cycle. (b) Laboratory cycle. (c) Endurance data for type II cycle. (d) Endurance data for laboratory cycle.
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Published: 01 December 1989
Fig. 4.16. Effect of tensile hold time at 600 °C (1110 °F) on cyclic endurance of 2¼Cr-1Mo steel ( Ref 38 ).
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Published: 01 December 1989
Fig. 4.18. Effect of tensile hold time on fatigue endurance of type 316 stainless steel ( Ref 41 ).
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Published: 01 December 1989
Fig. 4.23. Endurance curves for various types of cycles for cast IN-738 at 850 °C (1560 °F) ( Ref 65 and 66 ).
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Published: 01 December 1989
Fig. 4.26. Effect of ductility on endurance of ferritic steels ( Ref 20 ).
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Published: 01 March 2006
Fig. 3.13 Removal of an “apparent endurance limit” by occasional overstraining and then testing at stresses lower than the original endurance limit. Fatigue life becomes finite below the endurance limit. Source: Ref 3.16
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Published: 01 March 2006
Fig. 10.1 Endurance limit predictions for various steels based on calorimetric rise of temperature measurements. Data from Ref 10.5
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in Avoidance, Control, and Repair of Fatigue Damage[1]
> Fatigue and Durability of Structural Materials
Published: 01 March 2006
Fig. 11.70 The effect of one preload and of periodic high loads on endurance of aluminum alloy parts subjected to fluctuating tension. Source: Ref 11.77
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in Avoidance, Control, and Repair of Fatigue Damage[1]
> Fatigue and Durability of Structural Materials
Published: 01 March 2006
Fig. 11.74 Relative endurance of prenitrided and control-lot bearing inner rings. Source: Ref 11.81
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Published: 01 December 1999
Fig. 7.29 Relative variations in the (1) fatigue endurance limit, (2) fracture toughness parameter, and (3) 0.2% yield strength as a result of cold treatment at various temperatures. The relative change is a ratio of properties after treatment and properties prior to treatment. Source: Ref 45
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Published: 01 December 1999
Fig. 8.35 Shot peening improves endurance limits of ground parts. Reversed bending fatigue of flat bars of 45 HRC. Source: Ref 42
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in Mechanical Properties
> Powder Metallurgy Stainless Steels: Processing, Microstructures, and Properties
Published: 01 June 2007
Fig. 7.11 Tensile strength versus fatigue endurance limit of various powder metallurgy 400-series stainless steels. Source: Ref 33 . Reprinted with permission from SAE Paper 03M-315 ©2003 SAE International
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Published: 01 September 2005
Fig. 16 Endurance limits as a function of prior-austenite grain size from various studies of bending fatigue of gas-carburized 4320 steels. Source: Ref 28
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Published: 01 March 2006
Fig. 8.6 Effect of surface finish on endurance limit of steel. Source: Ref 8.6
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Published: 01 March 2006
Fig. 8.7 Reduction of endurance strength due to surface finish for steel. Source: Ref 8.6
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Published: 01 June 2008
Fig. 14.5 Endurance limit versus hardness for steels. Source: Ref 3
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in Melting, Casting, and Powder Metallurgy[1]
> Titanium: Physical Metallurgy, Processing, and Applications
Published: 01 January 2015
Fig. 8.25 Effect of density on the fatigue endurance limit of pressed-and-sintered Ti-6Al-4V
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Published: 01 October 2011
Fig. 10.25 Effect of tensile strength and matrix structure on endurance ratio for ductile iron
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