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fatigue strength
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Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 2005
DOI: 10.31399/asm.tb.mmfi.t69540121
EISBN: 978-1-62708-309-6
... their use on different metals and alloys. The chapter also discusses design-based approaches for preventing fatigue failures. crack initiation crack propagation fatigue analysis fatigue fracture appearance fatigue life fatigue strength THE DEFINITION OF “FATIGUE” according to ASTM Standard E...
Abstract
This chapter examines the stress-strain characteristics of metals and alloys subjected to cyclic loading and the cumulative effects of fatigue. It begins by explaining how a single load reversal can lower the yield stress of a material and how repeated reversals can cause strain hardening and softening, both of which lead to premature failure. It then discusses the stages of fatigue fracture, using detailed images to show how cracks initiate and grow and how they leave telltale marks on fracture surfaces. It goes on to describe fatigue life assessment methods and demonstrate their use on different metals and alloys. The chapter also discusses design-based approaches for preventing fatigue failures.
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in Fatigue and Fracture of Engineering Alloys
> Fatigue and Fracture<subtitle>Understanding the Basics</subtitle>
Published: 01 November 2012
Fig. 32 Relationships between the fatigue strength and tensile strength of some wrought aluminum alloys. Source: Ref 11
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in Modeling and Use of Correlations in Heat Treatment
> Principles of the Heat Treatment of Plain Carbon and Low Alloy Steels
Published: 01 December 1996
Fig. 9-27 Relation between the fatigue strength and the tensile strength for several steels. The straight lines have the slope shown. (Adapted from a compilation of T.J. Dola and C.S. Yen, Proc. ASTM , Vol 48, p 664 (1948), Ref 26 )
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in Modeling and Use of Correlations in Heat Treatment
> Principles of the Heat Treatment of Plain Carbon and Low Alloy Steels
Published: 01 December 1996
Fig. 9-28 The fatigue strength as a function of yield strength for steels. (From C.R. Brooks, The Heat Treatment of Ferrous Alloys , Hemisphere Publishing Corporation/McGraw-Hill Book Company, New York (1979), Ref 27 )
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Published: 01 July 1997
Fig. 6 Effect of material tensile strength or the fatigue strength of welded and unwelded specimens
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Published: 01 November 2012
Fig. 5 Influence of stress ratio R on fatigue strength. UTS, ultimate tensile strength; YS, yield strength. Source: Adapted from Ref 4
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Published: 01 November 2012
Fig. 50 Loss of fatigue strength from the abusive grinding of 4340 steel quenched and tempered to 50 HRC. UTM, untempered martensite. Source: Ref 27
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in Fatigue and Fracture of Engineering Alloys
> Fatigue and Fracture<subtitle>Understanding the Basics</subtitle>
Published: 01 November 2012
Fig. 30 Comparison of fatigue strength bands for 2014-T6, 2024-T4, and 7075-T6 aluminum alloys for rotating beam tests. Source: Ref 16
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in Fatigue and Fracture of Engineering Alloys
> Fatigue and Fracture<subtitle>Understanding the Basics</subtitle>
Published: 01 November 2012
Fig. 33 Axial stress fatigue strength of 0.8 mm (0.030 in.) 2024, 7075, and clad sheet in air and seawater, R = 0. Source: Ref 19
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in Metallic Joints: Mechanically Fastened and Welded
> Fatigue and Fracture<subtitle>Understanding the Basics</subtitle>
Published: 01 November 2012
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in Metallic Joints: Mechanically Fastened and Welded
> Fatigue and Fracture<subtitle>Understanding the Basics</subtitle>
Published: 01 November 2012
Fig. 2 Axial fatigue strength at 10 7 cycles of bolt-nut assemblies with rolled threads and machined threads ( R = –1). Source: Ref 2
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in Fatigue and Fracture of Continuous-Fiber Polymer-Matrix Composites
> Fatigue and Fracture<subtitle>Understanding the Basics</subtitle>
Published: 01 November 2012
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in Fatigue and Fracture of Continuous-Fiber Polymer-Matrix Composites
> Fatigue and Fracture<subtitle>Understanding the Basics</subtitle>
Published: 01 November 2012
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Published: 01 July 2009
Fig. 17.44 Comparison of fatigue-strength-to-density ratio of notched specimens of beryllium, titanium (Ti-6Al-4V), and aluminum (7075-T6). Source: Bush Wellman 2001
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Published: 01 July 2009
Fig. 17.45 Comparison of axial fatigue strength of smooth specimens of beryllium, titanium (Ti-6Al-4V), and aluminum (7075-T6). Source: Brush Wellman 2001
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Published: 01 October 2012
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Published: 01 October 2012
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Published: 01 October 2012
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Published: 01 November 2010
Fig. 1.17 Comparative notched fatigue strength of composite laminate and aluminum alloy sheet. Source: Ref 3
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Published: 01 December 1999
Fig. 5 Plots of shear-fatigue strength (from hardness) against plots of shear stresses, τ yz , in rolling-contact tests. Predicted and actual fatigue limit values are in close agreement for carburized steels but not for the four nitrided steels. Relative radius of curvature, 2/3. SH units = lb
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