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Residual stresses
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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.
Series: ASM Technical Books
Publisher: ASM International
Published: 01 June 2022
DOI: 10.31399/asm.tb.tstap.t56040084
EISBN: 978-1-62708-428-4
... Abstract This article, prepared under the auspices of the ASM Thermal Spray Society Committees on Accepted Practices, describes a procedure for evaluating residual stresses in thermal spray coatings, which is an extension of the well-known layer removal method to include the Young’s modulus...
Abstract
This article, prepared under the auspices of the ASM Thermal Spray Society Committees on Accepted Practices, describes a procedure for evaluating residual stresses in thermal spray coatings, which is an extension of the well-known layer removal method to include the Young’s modulus and Poisson’s ratio properties of the thermal spray coating material and the substrate. It presents questions and answers that were selected to introduce residual stresses in thermal spray coatings. The article describes equipment and the laboratory procedure for the modified layer removal method and provides the description of the residual stress specimen. It also describes the procedures for applying or installing bonded resistance strain gages, the dimensions of the test specimen, the procedure for removing layers, and the method for interpreting the data to evaluate residual stresses. The spreadsheet program, “ MLRM for Residual Stresses ,” is available as a supplement to this document.
Image
Published: 01 August 2005
Fig. 3.63 Demonstration of the principle of mechanically induced residual stresses. (a) A hard ball pressed into a metal surface at the point of greatest penetration. Note that the original surface (dashed line) is stretched (tension) into a spherical shape by the force on the ball. Radial
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Published: 01 August 2012
Fig. 16.17 Residual stresses caused by surface features in chemical vapor deposition or physical vapor deposition coating. (a) Ideal case. (b) Edge. (c) Coating edge. (d) Groove. (e) Ridge. Source: Ref 16.56
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in Stress-Corrosion Cracking of Aluminum Alloys[1]
> Stress-Corrosion Cracking<subtitle>Materials Performance and Evaluation</subtitle>
Published: 01 January 2017
Fig. 8.7 Comparison of residual stresses in a thick, constant cross-section 7075-T6 aluminum alloy plate before and after stress relief. (a) High residual stresses in the solution-treated and quenched alloy. (b) Reduction in stresses after stretching 2%. Source: Ref 8.18
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in Stress-Corrosion Cracking of Weldments in Boiling Water Reactor Service[1]
> Stress-Corrosion Cracking<subtitle>Materials Performance and Evaluation</subtitle>
Published: 01 January 2017
Fig. 15.4 Peak axial residual stresses on the inside surface of welded type 304 stainless steel pipes. Source: Ref 15.4
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in Stress-Corrosion Cracking of Weldments in Boiling Water Reactor Service[1]
> Stress-Corrosion Cracking<subtitle>Materials Performance and Evaluation</subtitle>
Published: 01 January 2017
Fig. 15.5 Through-wall distribution of weld residual stresses in a 660 mm (26 in.) diam type 304 stainless steel pipe. Source: Ref 15.7
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in Stress-Corrosion Cracking of Weldments in Boiling Water Reactor Service[1]
> Stress-Corrosion Cracking<subtitle>Materials Performance and Evaluation</subtitle>
Published: 01 January 2017
Fig. 15.7 Through-wall axial residual stresses for last-pass heat-sink welding (LPHSW) of a 610 mm (24 in.) diam type 304 stainless steel pipe. Source: Ref 15.12
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in Stress-Corrosion Cracking of Weldments in Boiling Water Reactor Service[1]
> Stress-Corrosion Cracking<subtitle>Materials Performance and Evaluation</subtitle>
Published: 01 January 2017
Fig. 15.8 Through-wall axial residual stresses in induction heating stress improvement (IHSI) treated and nontreated 410 mm (16 in.) diam type 304 stainless steel pipe weldments. Source: Ref 15.13
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in Evaluation of Stress-Corrosion Cracking[1]
> Stress-Corrosion Cracking<subtitle>Materials Performance and Evaluation</subtitle>
Published: 01 January 2017
Fig. 17.22 Stress-corrosion cracking test specimens containing residual stresses from plastic deformation. (a) Cracked cup specimen (Ericksen impression). Source: Ref 17.4 . (b) Joggled extrusion containing SCC in the plastically deformed region. Source: Ref 17.9
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in Evaluation of Stress-Corrosion Cracking[1]
> Stress-Corrosion Cracking<subtitle>Materials Performance and Evaluation</subtitle>
Published: 01 January 2017
Fig. 17.23 Stress-corrosion cracking test specimens containing residual stresses from plastic deformation. Shown are 12.7 mm (0.5 in.) diameter stainless tubular specimens after SCC testing. (a) and (b) Annealed tubing that was cold formed before testing. (c) Cold worked tubing tested
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in Evaluation of Stress-Corrosion Cracking[1]
> Stress-Corrosion Cracking<subtitle>Materials Performance and Evaluation</subtitle>
Published: 01 January 2017
Fig. 17.24 Stress-corrosion cracking test specimen containing residual stresses from welding. (a) Sandwich specimen simulating rigid structure. Note SCC in edges of center plate. Source: Ref 17.10 . (b) Cracked ring-weld specimen. Source: Ref 17.4
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Published: 01 September 2008
Fig. 96 Stress profile in a round bar in the loaded state, where residual stresses after induction surface hardening and loading stresses add up. Source: Ref 15
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Published: 01 September 2008
Fig. 97 Stress profile in a round bar in the loaded state, where residual stresses after carburizing or nitriding and loading stresses add up. Source: Ref 15
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Published: 01 August 2015
Fig. 5.24 Complex pattern of residual stresses forms in a carbon steel cylinder after induction heating and spray quenching. One of the goals of tempering is to relieve the subsurface tensile stresses that can cause cracking in service. Surface compressive stresses are beneficial. Stresses
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Published: 30 November 2013
Fig. 2 Thermal residual stresses. (a) Unrestrained expansion and contraction. (b) Restrained expansion, unrestrained contraction. (c) Restrained expansion and contraction.
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Published: 30 November 2013
Fig. 3 Deformation caused by thermal residual stresses. (a) Flat, platelike metal at uniform temperature. (b) Lateral expansion of upper part on heating is restrained by cold, strong metal below, causing compressive stress (C) on upper (convex) and lower (concave) surfaces and tensile stress
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Image
Published: 30 November 2013
Fig. 4 Thermal residual stresses caused by spot heating. (a) Stress-free plate or sheet at uniform temperature. (b) When locally through-heated, plate expands laterally, generating compressive stresses; also bulges in thickness direction. (c) When cooled to original temperature, plate
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Image
Published: 30 November 2013
Fig. 7 Demonstration of the principle of mechanically induced residual stresses. (a) A hard ball pressed into a metal surface at point of greatest penetration. Note that the original surface (dashed line) is stretched (tension) into a spherical shape by the force on the ball. Radial reaction
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