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cyclic stress
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Book: Fatigue and Fracture
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002354
EISBN: 978-1-62708-193-1
... Abstract This article discusses the microstructural processes that take place during plastic deformation and presents a plain phenomenological and general description of the cyclic stress-strain (CSS) response. It emphasizes the microstructural aspects of cyclic loading on single-phase...
Abstract
This article discusses the microstructural processes that take place during plastic deformation and presents a plain phenomenological and general description of the cyclic stress-strain (CSS) response. It emphasizes the microstructural aspects of cyclic loading on single-phase materials tested in initially soft, dislocation-poor conditions resulting from a prior heat treatment. The article discusses deformation-induced phase transformations in austenitic stainless steels and commercial age-hardened aluminum alloys. It describes the interaction of dislocations and the strengthening of second-phase particles. The article also provides a description of the framework used to model the CSS response on a physical basis.
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Published: 01 January 1996
Fig. 27 Cyclic stress intensity range, Δ K, vs. cyclic fatigue crack growth rate, Δ a /Δ N, of laboratory-fabricated high-strength 7XXX aluminum alloys
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Published: 30 November 2018
Fig. 8 Strain-controlled fatigue tests. Cyclic stress-strain curves for metal-matrix composite with alumina contents from 0 to 15%. AS, as-sintered; HT, heat treated, T6. Source: Ref 71
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Published: 01 June 2012
Fig. 22 Two examples of how cyclic stress-strain curves change during cycling. (a) Room-temperature, stress-controlled cycling of a martensitic structure (M s = +70 °C, or 160 °F). (b) Room-temperature, strain-controlled cycling of martensite (M s = 30 °C, or 85 °F). Both examples exhibit
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Published: 01 January 2003
Fig. 2 Nomenclature used to describe test parameters involved in cyclic stress testing. S a , stress amplitude; S m , mean stress; S r , stress range
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Published: 01 January 2000
Fig. 57 Schematic of the cyclic stress-strain behavior of a quasi-isotropic laminate of boron/aluminum as a function of number of cycles. Source: Ref 84
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Published: 01 January 2000
Fig. 58 The cyclic stress-strain response of a boron/aluminum ([0/±45/ 90 /0/±45/90] s , V f = 0.45) composite showing a dramatic change due to fatigue damage and cyclic hardening of the matrix material. (a) After 4 cycles. (b) After 500,000 cycles
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Published: 01 January 2001
Fig. 8 Cyclic stress-strain loops for a discontinuously reinforced composite compared to unreinforced matrix alloy. (a) Stress-controlled conditions. (b) Strain-controlled conditions. Source: Ref 45
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Published: 01 January 2000
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Published: 01 January 1996
Fig. 5 Monotonic and cyclic stress-strain curves for 4140 steel tempered at 400 °C (750 °F). Large cyclic softening is observed. The cyclic stress-strain curve was obtained by the incremental strain technique. Source: Ref 15
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Published: 01 January 1996
Fig. 12 Cyclic stress-strain curve of monocrystalline copper oriented for single slip. Source: Ref 38
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Published: 01 January 1996
Fig. 35 Cyclic stress-strain curves of annealed and prestrained copper specimens. Source: Ref 210
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Published: 01 January 1997
Fig. 17 Monotonic and cyclic stress-strain diagrams for six different engineering alloys. ○, companion specimens; solid line, incremental step. Source: Ref 35
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Published: 31 August 2017
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in Thermomechanical Fatigue: Mechanisms and Practical Life Analysis
> Failure Analysis and Prevention
Published: 01 January 2002
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Published: 01 January 2002
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Published: 01 December 2008
Fig. 18 Monotonic tensile and cyclic stress-strain behavior of comparable cast and wrought normalized-and-tempered carbon steels
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Published: 01 January 1996
Fig. 17 Cyclic stress vs. strain curves for 2 1 4 Cr-1Mo steel (class 2), derived from the stress amplitude at half life, at 450 and 550 °C. Strain rate 0.1% per second. R = −1. Source: Ref 22
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Published: 01 January 1996
Fig. 28 Effect of environment and cyclic stress intensity range on the growth rate of fatigue cracks in Type 304 stainless steel. Source: Ref 39
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Published: 01 January 1996
Fig. 12 Construction of cyclic stress-strain curve by joining tips of stabilized hysteresis loops
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