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elastic strain

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Published: 01 July 2009
Fig. 6.23 Schematic strain-strain flow diagram. Elastic strain range versus inelastic strain range for nonisothermal creep-fatigue cycles. Cyclic strain-hardening coefficient K IJ is shown as a decreasing function of hold-time per cycle, assuming constant n . Source: Ref 6.9 More
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Published: 01 November 2012
Fig. 22 Log elastic strain versus log reversals to failure. Source: Ref 11 More
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Published: 01 July 2009
Fig. 6.24 Schematic representation of the hold-time dependency of the elastic strain range versus cyclic life relationship for creep cycles. Value of intercept B is governed by Eq ( 6.15 ) Source: Ref 6.9 More
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Published: 01 July 2009
Fig. 6.34 Elastic strain range versus life relationship in Ref 6.6 for PP loading: René 95, 650 °C (1200 °F). Data from Ref 6.22 and 6.23 . Source: Ref 6.6 More
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Published: 01 July 2009
Fig. 6.35 Time-dependent intercepts for elastic strain range versus life relationships reported in Ref 6.6 ; René 95, 650 °C (1200 °F). Data from Ref 6.22 and 6.23 . Source: Ref 6.6 More
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Published: 01 December 2004
Fig. 3 A relationship between elastic and anelastic strains. The elastic strains develop as soon as the load is applied, whereas the anelastic strains are time dependent. More
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Published: 01 March 2006
Fig. A.35 Stress-strain curves featuring (a) linear elastic response, (b) elastic plus plastic response, and (c) elastic plus creep response More
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Published: 01 November 2012
Fig. 4 Typical stress-strain diagram showing different regions of elastic and plastic behavior. (a) Elastic region in which original size and shape will be restored after release of load. (b) Region of permanent deformation but without localized necking. (c) Region of permanent deformation More
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Published: 01 August 2012
Fig. 2.13 Distribution of (a) strain and (b) stress in an elastic, perfectly plastic sheet bent to a gentle curvature and stretched. Source: Ref 2.10 More
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Published: 01 August 2005
Fig. 3.45 Elastic, plastic, and total strain range as a function of life for a low-carbon martensitic steel. Source: Ref 3.41 More
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Published: 01 August 2005
Fig. 2.7 Schematic elastic and inelastic strain. Source: Ref 2.4 More
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Published: 01 July 2009
Fig. 14.10 Composite stress-strain behavior based on the moduli and elastic limits. A: beryllium elastic limit; B: composite elastic limit; I: fully elastic; II: elastic plastic; C: unloading point. Source: London et al. 1979 More
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Published: 01 December 2004
Fig. 2 Stress-strain behavior in the region of the elastic limit. (a) Definition of σ and ε in terms of initial test piece length, L , and cross-sectional area, A 0 , before application of a tensile force, F. (b) Stress-strain curve for small strains near the elastic limit (EL) More
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Published: 01 December 2004
Fig. 1 Schematic representation of the elastic portions of the stress-strain curves for iron, copper, and aluminum More
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Published: 01 December 1989
Fig. 4.12. Fatigue life as a function of elastic, plastic, and total strain amplitude. More
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Published: 01 October 2011
Fig. 5 Elastic-plastic material response, shown as a uniaxial tensile strain More
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Published: 30 November 2013
Fig. 1 General stress-strain curve showing elastic and plastic portions of a typical curve. Area marked “Yield” is the area of transition from elastic to plastic deformation. Yield strength, yield point, elastic limit, and proportional limit are all in this area. See Glossary for specific More
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Published: 30 November 2013
Fig. 4 Typical stress-strain diagram showing different regions of elastic and plastic behavior. (a) Elastic region in which original size and shape will be restored after release of load. (b) Region of permanent deformation but without localized necking. (c) Region of permanent deformation More
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Published: 01 July 2009
Fig. 6.21 Construction of inelastic, elastic, and total strain-range life relationships for tensile strain hold-time cycling More
Series: ASM Technical Books
Publisher: ASM International
Published: 01 July 2009
DOI: 10.31399/asm.tb.fdmht.t52060111
EISBN: 978-1-62708-343-0
... Abstract This chapter explains why it is sometimes necessary to separate inelastic from elastic strains and how to do it using one of two methods. It first discusses the direct calculation of strain-range components from experimental data associated with large strains. It then explains how...