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Published: 01 January 1990
Fig. 25 Typical thermal stress cycles at the beginning of the test for FG and CG irons. Source: Ref 23 More
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Published: 01 January 1990
Fig. 26 The shift in thermal stress versus the number of cycles for six irons cycled between 100 and 540 °C (212 and 1000 °F). Source: Ref 23 More
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Published: 09 June 2014
Fig. 8 Coupling of electromagnetic, thermal, stress, and phase-transformation models into DANTE model to simulate induction hardening processes. Source: Ref 8 More
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Published: 31 August 2017
Fig. 21 Typical thermal stress cycles at the beginning of the test for flake graphite and compacted graphite (CG) irons. Source: Ref 18 More
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Published: 31 August 2017
Fig. 22 The shift in thermal stress versus the number of cycles for six irons cycled between 100 and 540 °C (212 and 1000 °F). CG, compacted graphite. Source: Ref 18 More
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Published: 01 February 2024
Fig. 5 Schematic of time-dependent variation of thermal stress in the longitudinal direction during quenching of a steel bar, and residual stress distribution in the longitudinal direction. Source: Ref 9 More
Series: ASM Handbook
Volume: 11B
Publisher: ASM International
Published: 15 May 2022
DOI: 10.31399/asm.hb.v11B.a0006932
EISBN: 978-1-62708-395-9
... Abstract Engineering plastics, as a general class of materials, are prone to the development of internal stresses which arise during processing or during servicing when parts are exposed to environments that impose deformation and/or temperature extremes. Thermal stresses are largely...
Book Chapter

Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.a0003136
EISBN: 978-1-62708-199-3
... Abstract Copper and copper alloys are used extensively in structural applications in which they are subject to moderately elevated temperatures. At relatively low operating temperatures, these alloys can undergo thermal softening or stress relaxation, which can lead to service failures...
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Published: 01 January 2002
Fig. 10 Development of thermal stresses within steel on cooling. T, time instant at maximum temperature difference; 0, time instant of stress reversal; curve A, stress variation at the surface under elastic conditions. B and C are actual thermal stress variations at the surface and the core More
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Published: 30 September 2014
Fig. 17 Development of thermal stresses on cooling. Source: Ref 19 More
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Published: 01 August 2013
Fig. 40 Formation of thermal stresses on cooling in a 100 mm (4 in.) steel specimen. C designates the core, S the surface, u the stress reversal time instant, and w the time instant of maximum temperature difference. The top graph shows the temperature variation with time at the surface More
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Published: 30 September 2014
Fig. 15 Creation of thermal stresses. C, core; S, surface. Source: Ref 13 More
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Published: 01 January 1994
Fig. 3 Calculated thermal stresses for thin coatings on high-performance carbon-carbon laminates. Ratio of substrate thickness to coating thickness = 20 More
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Published: 01 January 2001
Fig. 9 Calculated thermal stresses for thin coatings on high-performance carbon-carbon laminates. Ratio of substrate thickness to coating thickness = 20. More
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Published: 01 November 2010
Fig. 56 Formation of thermal stresses on cooling in a 100 mm (4 in.) steel specimen. C designates the core, S the surface, u the instant of stress reversal, and w the time instant of maximum temperature difference. The top graph shows the temperature variation with time at the surface More
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Published: 01 November 2010
Fig. 82 Three typical theoretical examples of thermal stresses and plastic strains in ingot cores during the heating process of high-carbon-chromium steel ingots during heating. (Subscripts r, t, and z are radial, tangential, and axial stresses and strains, respectively.) Source: Ref 178 More
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Published: 15 June 2020
Fig. 37 Visible macrolevel cracks due to hoop and axial thermal stresses on as-built SLM cobalt-chrome alloy More
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Published: 01 November 1995
Fig. 14 Calculated thermal stresses for thin coatings on high-performance carbon-carbon laminates. Ratio of substrate thickness to coating thickness = 20. More
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Published: 01 January 2000
Fig. 4 Distribution of normalized thermal stresses in a pressurized tube with a ratio of inner radius, R i , to outer radius, R o , of 0.6 and with a temperature gradient of 50 °C (90 °F) under external heating More
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Published: 01 January 2002
Fig. 37 Stainless steel superheater tube that failed by thermal fatigue and stress rupture. (a) Photograph of the tube showing thick-lip rupture. (b) Macrograph of a section taken transverse to a fracture surface of the tube showing that thermal fatigue cracking started at the outside surface More