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low cycle fatigue
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in High-Entropy Alloys
> Mechanical Behavior of High-Entropy Alloys: Key Topics in Materials Science and Engineering
Published: 01 February 2022
Fig. 4 The illustration of high-cycle and low-cycle fatigue; the inset figure is the fatigue-loading cycles. Source: Ref 60
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Published: 01 December 1989
Fig. 4.24. Variation of number of cycles to failure (N f ) in low-cycle fatigue as a function of inelastic strain range and frequency ( ν ) for MAR-M 509 ( Ref 67 ).
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Published: 01 December 1989
Fig. 4.25. Effect of rupture ductility on hold-time effects during low-cycle fatigue testing of 1Cr-Mo-V rotor steel ( Ref 68 ).
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Published: 01 December 1989
Fig. 4.28. Creep-rupture/low-cycle-fatigue damage interaction curve for 1Cr-Mo-V rotor steel at 540 °C (1000 °F) (after Ref 82 ).
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in Life Assessment of Steam-Turbine Components
> Damage Mechanisms and Life Assessment of High-Temperature Components
Published: 01 December 1989
Fig. 6.12. Low-cycle-fatigue curves for Cr-Mo-V rotor steels at approximately 540 °C (1000 °F) ( Ref 22 ).
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in Life Assessment of Steam-Turbine Components
> Damage Mechanisms and Life Assessment of High-Temperature Components
Published: 01 December 1989
Fig. 6.53. Low-cycle-fatigue behavior of steam-turbine bolt materials at high temperature ( Ref 121 ).
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in Materials for Advanced Steam Plants
> Damage Mechanisms and Life Assessment of High-Temperature Components
Published: 01 December 1989
Fig. 8.21. Mean low-cycle-fatigue curves for 1Cr-Mo-V and 12Cr-Mo-V rotors compared with data on ESR 12Cr-Mo-V steel from Kobe Steel (based on Ref 67 and 71 ). For ESR 12Cr-Mo-V steel (crosshatched area), ○ denotes room temperature and Δ denotes 550 to 600 °C (1020 to 1110 °F).
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in Materials for Advanced Steam Plants
> Damage Mechanisms and Life Assessment of High-Temperature Components
Published: 01 December 1989
Fig. 8.26. Comparison of low-cycle fatigue behavior of 3.5Ni-Cr-Mo-V rotor steel in superclean and normal conditions ( Ref 82 ).
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in Life-Assessment Techniques for Combustion Turbines
> Damage Mechanisms and Life Assessment of High-Temperature Components
Published: 01 December 1989
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in Life-Assessment Techniques for Combustion Turbines
> Damage Mechanisms and Life Assessment of High-Temperature Components
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 ).
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in Failure of a High-Pressure Turbine Blade in an Aircraft Engine
> Failure Analysis of Engineering Structures: Methodology and Case Histories
Published: 01 October 2005
Fig. CH31.3 (a) SEM fractograph showing low-cycle fatigue striations in zone 2. (b) SEM fractograph showing the transition from fatigue to intercrystalline fracture. Arrows indicate the transition.
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Published: 01 December 2000
Fig. 12.21 Low-cycle fatigue life of Ti-6Al-4V alpha-beta titanium alloy with different structures: beta forged (100% transformed beta); 10% primary alpha (balance transformed beta); 50% primary alpha
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Published: 01 December 2000
Fig. 12.22 Effects of surface condition on low-cycle fatigue life of Ti-6Al-4V at 21 °C (70 °F)
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Published: 01 December 2000
Fig. 12.23 Low-cycle fatigue properties of alpha-beta titanium alloy Ti-6Al-4V showing effects of notch acuity and time to first crack
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Published: 01 March 2002
Fig. 12.46 Low-cycle fatigue behavior of IN 738 nickel-base superalloy in vacuum, air, and hot corrosion environments at 899 °C (1650 °F) and two cycling rates
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Published: 01 March 2002
Fig. 14.19 Low-cycle fatigue cracking induced by thermal strains in the rivet slot of a nickel-base superalloy disk
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in Life-Assessment Techniques for Combustion Turbines
> Damage Mechanisms and Life Assessment of High-Temperature Components
Published: 01 December 1989
Fig. 9.13. (a) Typical fatigue cycles employed for, and (b) results of low-cycle-fatigue tests on, cast IN 738 LC ( Ref 12 and 20 ).
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Published: 30 November 2013
Fig. 10 Schematic showing the relationship between low- and high-cycle fatigue. In systems where significant vibration loads are present, high-cycle fatigue (HCF) tends to be related to high-frequency loading, and low-cycle fatigue (LCF) tends to be related to slowly applied higher-stress
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Published: 01 December 1995
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
..., 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...
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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