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Published: 01 January 1996
Image
Effects of both initial and periodic overstrain on the strain-life curve fo...
Available to PurchasePublished: 01 January 1996
Fig. 14 Effects of both initial and periodic overstrain on the strain-life curve for an alloy steel. The fatigue limit for the no overstrain case is estimated from test data on similar material. From Ref 1 (p 666) as based on data from Ref 15
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Published: 01 January 2000
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Published: 01 January 1996
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Strain-life curves for a steel at three different hardness levels (approxim...
Available to PurchasePublished: 01 January 1996
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Strain-life curves for steels with varying microstructures and hardnesses. ...
Available to PurchasePublished: 01 January 1996
Fig. 25 Strain-life curves for steels with varying microstructures and hardnesses. Source: Ref 6
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Strain-life curves for samples of 7050 alloy with shearable precipitates (4...
Available to PurchasePublished: 01 January 1996
Fig. 35 Strain-life curves for samples of 7050 alloy with shearable precipitates (4 h at 120 °C, or 250 °F) and nonshearable precipitates (96 h at 150 °C, or 300 °F)
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Image
Published: 01 January 1996
Fig. 36 Strain-life curves for samples of Al-Zn-Mg- x Cu alloys with shearable precipitates (0.01% Cu) and nonshearable precipitates (2.1% Cu). DR, degree of recrystallization. (a) Cycled in dry air. (b) Cycled in distilled water. Source: Ref 64
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Image
Strain-life curves of large-grained Al-Zn-Mg alloy with shearable precipita...
Available to PurchasePublished: 01 January 1996
Fig. 42 Strain-life curves of large-grained Al-Zn-Mg alloy with shearable precipitates when underaged (4 h at 120 °C, or 250 °F) and nonshearable precipitates plus PFZs when overaged (96 h at 150 °C, or 300 °F). Source: Ref 64
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Strain-life curves for samples of 7050 alloy with shearable precipitates (4...
Available to PurchasePublished: 15 June 2019
Fig. 26 Strain-life curves for samples of 7050 alloy with shearable precipitates (4 h at 120 °C, or 250 °F) and nonshearable precipitates (96 h at 150 °C, or 300 °F)
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Image
Strain-life curves for samples of Al-Zn-Mg- x Cu alloys with shearable prec...
Available to PurchasePublished: 15 June 2019
Fig. 27 Strain-life curves for samples of Al-Zn-Mg- x Cu alloys with shearable precipitates (0.01% Cu) and nonshearable precipitates (2.1% Cu). DR, degree of recrystallization. (a) Cycled in dry air. (b) Cycled in distilled water
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Image
Strain-life curves of large-grained Al-Zn-Mg alloy with shearable precipita...
Available to PurchasePublished: 15 June 2019
Fig. 33 Strain-life curves of large-grained Al-Zn-Mg alloy with shearable precipitates when underaged (4 h at 120 °C, or 250 °F) and nonshearable precipitates plus precipitate-free zones when overaged (96 h at 150 °C, or 300 °F)
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Published: 01 January 1996
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Published: 01 January 1996
Fig. 35 Strain-life fatigue curve of x 2080-T4 composite with and without reinforcement. Stress controlled, R = −1, at room temperature. Source: Ref 73
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Typical strain-life fatigue curve showing elastic and plastic components, a...
Available to Purchase
in Fatigue, Creep Fatigue, and Thermomechanical Fatigue Life Testing
> Mechanical Testing and Evaluation
Published: 01 January 2000
Fig. 22 Typical strain-life fatigue curve showing elastic and plastic components, annealed 4340 steel
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Derivation of the strain-life fatigue curve adjusted for mean stress effect...
Available to PurchasePublished: 30 August 2021
Fig. 23 Derivation of the strain-life fatigue curve adjusted for mean stress effects. Adapted from Ref 4
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Book Chapter
Fundamentals of Modern Fatigue Analysis for Design
Available to PurchaseBook: Fatigue and Fracture
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002364
EISBN: 978-1-62708-193-1
... instabilities caused by cyclic deformations. It discusses the effect of mean stress on fatigue life and presents the analysis of cumulative fatigue damage. The article concludes with examples of application techniques for fatigue life prediction. cyclic deformation cyclic stress-strain curve fatigue...
Abstract
Fatigue crack initiation is an important aspect of materials performance in design. This article summarizes some fundamental concepts and procedures for the fatigue life prediction of relatively homogeneous, wrought metals when a major portion of total life is exhausted in crack initiation. It presents an overview of the strain-based, as opposed to stress-based, criterion of material behavior and fatigue analysis. The article describes the cyclic stress-strain behavior of metals to illustrate the inadequacy of the monotonic or tensile stress-strain curve in accounting for material instabilities caused by cyclic deformations. It discusses the effect of mean stress on fatigue life and presents the analysis of cumulative fatigue damage. The article concludes with examples of application techniques for fatigue life prediction.
Book: Fatigue and Fracture
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002365
EISBN: 978-1-62708-193-1
... Abstract This article discusses two major approaches in estimating fatigue life from the viewpoint of their use as engineering methods. These include the stress-based (S-N curve) approach and strain-based approach. The stress-based and strain-based approaches are compared, with some comments...
Abstract
This article discusses two major approaches in estimating fatigue life from the viewpoint of their use as engineering methods. These include the stress-based (S-N curve) approach and strain-based approach. The stress-based and strain-based approaches are compared, with some comments on their manner of use and limitations. The use of the Palmgren-Miner rule for life prediction for variable amplitude loading is also discussed.
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Comparison of typical fatigue-life curves of ductile, gray, and compacted g...
Available to PurchasePublished: 31 August 2017
Fig. 34 Comparison of typical fatigue-life curves of ductile, gray, and compacted graphite irons. (a) Stress-life curves. (b) Strain-life curves. Source: Ref 53
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Image
Published: 01 January 1996
Fig. 13 Effect of initial overstrain (10 cycles at ε a = 0.02) on the strain-life curve of an aluminum alloy. Adapted from Ref 13 as based on data from Ref 14
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