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residual stress
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Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 30 November 2013
DOI: 10.31399/asm.tb.uhcf3.t53630035
EISBN: 978-1-62708-270-9
... Abstract Residual, or locked-in internal, stresses are regions of misfit within a metal part or assembly that can cause distortion and fracture just as can the more obvious applied, or service, stresses. This chapter describes the fundamental facts about residual stresses and discusses...
Abstract
Residual, or locked-in internal, stresses are regions of misfit within a metal part or assembly that can cause distortion and fracture just as can the more obvious applied, or service, stresses. This chapter describes the fundamental facts about residual stresses and discusses the basic mechanisms of residual stress formation: thermal, transformational, mechanical, and chemical.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 January 2015
DOI: 10.31399/asm.tb.spsp2.t54410487
EISBN: 978-1-62708-265-5
... Temperature and deformation gradients developed in the course of manufacturing can have undesired effects on the microstructures along their path; the two most common being residual stress and distortion. This chapter discusses these manufacturing-related problems and how they can be minimized...
Abstract
Temperature and deformation gradients developed in the course of manufacturing can have undesired effects on the microstructures along their path; the two most common being residual stress and distortion. This chapter discusses these manufacturing-related problems and how they can be minimized by heat treatments. It also provides information on residual stress evaluation and prediction techniques.
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Published: 01 December 2006
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Published: 01 December 1999
Fig. 7.19 Relationship between impact-fracture stress and compressive-residual stress (percent values indicate maximum amount of retained austenite content in the carburized case). Source: Ref 31
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in Annealing, Normalizing, Martempering, and Austempering
> Principles of the Heat Treatment of Plain Carbon and Low Alloy Steels
Published: 01 December 1996
Fig. 7-7 Residual stress as a function of stress relief annealing temperature and time. (From A.H. Rosenstein, J. Materials , Vol 6, p 265 (1971), Ref 4 )
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in Annealing, Normalizing, Martempering, and Austempering
> Principles of the Heat Treatment of Plain Carbon and Low Alloy Steels
Published: 01 December 1996
Fig. 7-8 Residual stress as a function of a parameter of stress relief annealing time and temperature. T is temperature in Rankine and t is time in hours. (From same source as Fig. 7-7 )
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in Avoidance, Control, and Repair of Fatigue Damage[1]
> Fatigue and Durability of Structural Materials
Published: 01 March 2006
Fig. 11.55 Residual stress and cold-work distributions in Inconel 718 after various surface treatments. (a) In-plane residual stress distribution. (b) Cold work-distribution. SP, shot peening; LPB, low-plasticity burnishing; LSP, laser shock peening. Source: Ref 11.68
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in Avoidance, Control, and Repair of Fatigue Damage[1]
> Fatigue and Durability of Structural Materials
Published: 01 March 2006
Fig. 11.56 General form of residual stress distribution induced by shot peening or similar surface cold working treatments. Source: Ref 11.60
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in Avoidance, Control, and Repair of Fatigue Damage[1]
> Fatigue and Durability of Structural Materials
Published: 01 March 2006
Fig. 11.71 Illustration of crack growth arrest by residual stress due to overload. A, slotted notch; B, crack developed at 65 ksi; C, tensile portion of fracture; D, crack developed at 20 ksi. Source: Ref 11.78
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in Avoidance, Control, and Repair of Fatigue Damage[1]
> Fatigue and Durability of Structural Materials
Published: 01 March 2006
Fig. 11.73 Residual stress in prenitrided and shot-peened ball bearing inner rings. Source: Ref 11.80
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Published: 01 December 1999
Fig. 6.14 Dependence of residual stress in carburized and hardened cases on core carbon level. (a) Residual stress distribution in samples of Cr-Mn-Ti steel of varying core carbon contents; case depth, 1.2 mm; quenched from 810 °C. (b) Relationship between surface residual stress and core
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Published: 01 December 1999
Fig. 6.15 Relationship between fatigue limit and surface residual stress for the Cr-Mn-Ti steel referred to in Fig. 6.14 . Generally (a) A reduction in surface compressive stresses leads to (b) A reduction in bending fatigue resistance. Source: Ref 13 , 15
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Published: 01 December 1999
Fig. 6.34 Effect of case depth on residual stress. Influence of internal oxidation at the surface of the deep-case test piece is also indicated. Source: Ref 40
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Published: 01 December 1999
Fig. 6.35 Effect of case depth on residual stress. Effect of carbon potential is also indicated. Source: Ref 41
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Published: 01 December 1999
Fig. 7.14 Variation of fatigue-crack initiation lives with residual stress at the notch of tested steels. Source: Ref 27
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Published: 01 December 1999
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Published: 01 December 1999
Fig. 8.12 Effect of the number of grinding passes on the residual stress distribution in case-hardened strips with a case depth of 1.6 to 1.7 mm. Source: Ref 16
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Published: 01 December 1999
Fig. 8.13 Influence of wheel condition on the residual stress distribution. Infeeds (mm) and feed rates (mm/rev) for the used wheel were less than those for the newly dressed wheel. ax, axial; tg, tangential
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Published: 01 December 1999
Fig. 8.23 Effect of rolling speed on the residual stress distribution at the surface of a 0.45% C steel. Source: Ref 26
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Published: 01 December 1999
Fig. 8.31 Effect of shot peening on the residual stress distortion in 20KhNM steel rings (case depth, 1 mm). Source: Ref 33
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