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fatigue endurance limits
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Image
Published: 01 October 2011
Fig. 17.6 Fatigue endurance limit vs. tensile strength for notched and unnotched cast and wrought carbon steels with various heat treatments. Data obtained in R.R. Moore rotating-beam fatigue tests with theoretical stress-concentration factor = 2.2
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in Melting, Casting, and Powder Metallurgy[1]
> Titanium: Physical Metallurgy, Processing, and Applications
Published: 01 January 2015
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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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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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in Carbon and Low Alloy Steels for Pressure Containing and Structural Parts
> Steel Castings Handbook
Published: 01 December 1995
Fig. 18-17 Relation between fatigue endurance limit (both notched and unnotched) and unnotched tensile strength for a number of cast and wrought steels with various heat treatments ( 13 )
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Published: 01 December 1999
, HRC Effective case depth (b) Impact fracture stress Fatigue endurance limit mm in. MPa ksi MPa ksi Carburized Unpeened 60.5 35 1.1 0.044 2240 325 730 105 SAE 4028 Shot peened 62.2 36 1.1 0.044 2265 329 1035 150 (a) Converted from HRA. (b) Distance
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in Attributes of Advanced High-Strength Steels
> Advanced-High Strength Steels: Science, Technology, and Applications
Published: 01 August 2013
Fig. 4.5 S - N curve showing fatigue characteristics and endurance limit of a metal displaying a fatigue limit. Source: Adapted from Ref 4.5
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in Fatigue and Fracture of Engineering Alloys
> Fatigue and Fracture<subtitle>Understanding the Basics</subtitle>
Published: 01 November 2012
Fig. 31 Fatigue ratios (endurance limit/tensile strength) for aluminum alloys and other materials. Source: Ref 18
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Published: 01 December 1995
Fig. 3-41 Anisotropy exhibited by fatigue strength and endurance limit in SAE 4340 forged steel ( 7 )
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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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in Introduction to Fatigue and Fracture
> Fatigue and Fracture<subtitle>Understanding the Basics</subtitle>
Published: 01 November 2012
Fig. 1 The process of fatigue. (a) Cyclic loading. (b) Fatigue life of steel with an endurance limit and aluminum with no endurance limit. Source: Ref 2
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Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 June 2008
DOI: 10.31399/asm.tb.emea.t52240243
EISBN: 978-1-62708-251-8
... at a specified stress level, while the fatigue strength (also referred to as the endurance limit) is the stress below which failure does not occur. As the applied stress level is decreased, the number of cycles to failure increases. Normally, the fatigue strength increases as the static tensile strength...
Abstract
Fatigue failures occur due to the application of fluctuating stresses that are much lower than the stress required to cause failure during a single application of stress. This chapter describes three basic factors that cause fatigue: a maximum tensile stress of sufficiently high value, a large enough variation or fluctuation in the applied stress, and a sufficiently large number of cycles of the applied stress. The discussion covers high-cycle fatigue, low-cycle fatigue, and fatigue crack propagation. The chapter then discusses the stages where fatigue crack nucleation and growth occurs. It describes the most effective methods of improving fatigue life. The chapter also explains the effect of geometrical stress concentrations on fatigue. In addition, it explores the environmental effects of corrosion fatigue, low-temperature fatigue, high-temperature fatigue, and thermal fatigue. Finally, the chapter discusses a number of design philosophies or methodologies to deal with design against fatigue failures.
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Published: 01 December 1999
Fig. 3.15 Bending fatigue S-N curves at a stress ratio of R = 0.1 for (a) Vacuum-A showing an endurance limit of 1370 MPa (200 ksi) and for (b) Vacuum-B showing an endurance limit of 1235 MPa (180 ksi). Considerable scatter in the data exists for both Vacuum-A and Vacuum-B conditions. Carbides
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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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Published: 01 December 2003
Fig. 2 Stress-number of cycles to fatigue ( S - N ) behavior of 400 specimens of EN-24 steel tested near the endurance limit. Source: Ref 5
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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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Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 2013
DOI: 10.31399/asm.tb.ahsssta.t53700071
EISBN: 978-1-62708-279-2
.... Fatigue characteristics are measured, plotted, and presented in the form of an S - N curve where S is the stress amplitude and N is the number of cycles to failure. Figure 4.5 shows a typical S - N curve on which the location of the endurance limit, σ e , of the metal is superimposed...
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2012
DOI: 10.31399/asm.tb.ffub.t53610147
EISBN: 978-1-62708-303-4
... has an endurance limit. In other words, below a certain stress level, the steel alloy will never fail. On the other hand, aluminum does not have a true endurance limit. It will always fail if tested to a sufficient number of cycles. Therefore, the fatigue strength of aluminum is usually reported...
Abstract
This chapter discusses the factors that play a role in fatigue failures and how they affect the service life of metals and structures. It describes the stresses associated with high-cycle and low-cycle fatigue and how they differ from the loading profiles typically used to generate fatigue data. It compares the Gerber, Goodman, and Soderberg methods for predicting the effect of mean stress from bending data, describes the statistical nature of fatigue measurements, and explains how plastic strain causes cyclic hardening and softening. It discusses the work of Wohler, Basquin, and others and how it led to the development of a strain-based approach to fatigue and the use of fatigue strength and ductility coefficients. It reviews the three stages of fatigue, beginning with crack initiation followed by crack growth and final fracture. It explains how fracture mechanics can be applied to crack propagation and how stress concentrations affect fatigue life. It also discusses fatigue life improvement methods and design approaches.
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 1995
DOI: 10.31399/asm.tb.sch6.t68200233
EISBN: 978-1-62708-354-6
... Strength (Endurance Limit) For cast steels, the fatigue strength, or endurance limit, as determined by tests on smooth bars is generally in the range of 40% to 50% of the tensile strength. In nonpercentage terms, this relationship is expressed as 0.40 to 0.50 and is termed the endurance ratio...
Abstract
The design stresses for most pressure-containing structural application, which are based upon minimum mechanical properties designated in the specifications published by the American Society for Testing and Materials (ASTM). This chapter reviews metallurgical characteristics and their influence on the properties and performance of structural carbon and low alloy steels and contains a summary of the relevant features of the ASTM product specifications.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.tb.aacppa.t51140055
EISBN: 978-1-62708-335-5
... × 10 5 2.1 × 10 5 Average 1.45 × 10 5 3.33 × 10 5 130% Average increase in fatigue life at 20 ksi (138 MPa) 202% (a) Casting process and part shape if known; PM, permanent mold. (b) Percent improvement by HIP in fatigue strength or endurance limit...
Abstract
Hot isostatic pressing (HIP) is a process refinement available to address internal porosity in castings. The HIP process may be used, in particular, for applications requiring very high quality and performance. This chapter discusses the principles, advantages, and disadvantages of HIP. It describes the effect of HIP on tensile properties and on the fatigue performance of aluminum alloy castings. In addition, the chapter discusses the processes involved in radiographic inspection of HIP-processed castings.
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