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Stress corrosion tests
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Image
Published: 01 January 2000
Fig. 6 Specimens for atmospheric stress-corrosion tests. (a) U-beam specimen. (b) Bent-beam specimen. (c) Direct tension specimen. (d) C-ring specimen
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Image
Published: 01 August 1999
Fig. 17 Crack propagation rates in stress-corrosion tests using precracked specimens of high-strength 2 xxx series aluminum alloys, 25 mm thick, double antilever beam, T-L (S-L) orientation of plate, wet twice a day with an aqueous solution of 3.5% NaCl, 23 °C. Source: Ref 13
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Image
Published: 01 August 1999
Fig. 20 Crack propagation rates in stress corrosion tests using 7 xxx series aluminum alloys, 25 mm thick, double cantilever beam (DCB), short-transverse orientation of die transverse orientation of die forgings and plate, alternate immersion tests, 23 °C. Source: Ref 13
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Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 January 2017
DOI: 10.31399/asm.tb.sccmpe2.t55090443
EISBN: 978-1-62708-266-2
... Abstract ASTM and other standards organizations have developed a number of tests for evaluating stress-corrosion cracking (SCC) under various conditions. This appendix lists many of the SCC tests that have been approved for specific materials and operating environments. stress corrosion...
Image
Published: 01 December 2008
Fig. 29 Constant load stress corrosion cracking (SCC) tests in aerated MgCl 2 at 150 °C. Source: Ref 5
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Series: ASM Technical Books
Publisher: ASM International
Published: 01 January 2017
DOI: 10.31399/asm.tb.sccmpe2.9781627082662
EISBN: 978-1-62708-266-2
Series: ASM Technical Books
Publisher: ASM International
Published: 01 January 2017
DOI: 10.31399/asm.tb.sccmpe2.t55090221
EISBN: 978-1-62708-266-2
..., microstructure, heat treatment, cold working, and stress intensity. It also provides information on stress-corrosion testing, mitigation techniques, and basic cracking mechanisms. cold working copper alloys stress-corrosion cracking stress-corrosion test THE PHENOMENON of stress-corrosion cracking...
Abstract
This chapter describes the conditions under which copper-base alloys are susceptible to stress-corrosion cracking (SCC) and some of the environmental factors, such as temperature, pH, and corrosion potential, that influence crack growth and time to failure. It explains that, although most of the literature has been concerned with copper zinc alloys in ammoniacal solutions, there are a number of alloy-environment combinations where SCC has been observed. The chapter discusses several of these cases and the effect of various application parameters, including composition, microstructure, heat treatment, cold working, and stress intensity. It also provides information on stress-corrosion testing, mitigation techniques, and basic cracking mechanisms.
Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 July 2000
DOI: 10.31399/asm.tb.fec.t65940451
EISBN: 978-1-62708-302-7
..., Test Method for Coulometric Reduction of Surface Films on Metallic Test Samples • B 826, Test Method for Monitoring Atmospheric Corrosion Tests by Electrical Resistance Probes • C 692, Method of Evaluating the Influence of Wicking-Type Thermal Insulations on the Stress Corrosion Cracking...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 January 2017
DOI: 10.31399/asm.tb.sccmpe2.t55090367
EISBN: 978-1-62708-266-2
... Abstract This chapter addresses the challenge of selecting an appropriate stress-corrosion cracking (SCC) test to evaluate the serviceability of a material for a given application. It begins by establishing a generic model in which SCC is depicted in two stages, initiation and propagation...
Abstract
This chapter addresses the challenge of selecting an appropriate stress-corrosion cracking (SCC) test to evaluate the serviceability of a material for a given application. It begins by establishing a generic model in which SCC is depicted in two stages, initiation and propagation, that further subdivide into several zones plus a transition region. It then discusses SCC test standards before describing basic test objectives and selection criteria. The chapter explains how to achieve the required loading conditions for different tests and how to prepare test specimens to determine elastic strain, plastic strain, and residual stress responses. It also describes the difference between smooth and precracked specimens and how they are used, provides information on slow-strain-rate testing and how to assess the results, and discusses various test environments and procedures, including tests for weldments. The chapter concludes with a section on how to interpret time to failure, threshold stress, percent survival, stress intensity, and propagation rate data, and assess the precision of the associated tests.
Image
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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Image
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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Image
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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Book Chapter
Series: ASM Technical Books
Publisher: ASM International
Published: 01 August 1999
DOI: 10.31399/asm.tb.caaa.t67870219
EISBN: 978-1-62708-299-0
... Abstract This chapter describes the use of standardized tests to determine the susceptibility of aluminum alloys to specific forms of corrosion, including pitting, intergranular corrosion, filiform corrosion, exfoliation corrosion, and stress-corrosion cracking. aluminum alloys corrosion...
Book Chapter
Book: Corrosion of Weldments
Series: ASM Technical Books
Publisher: ASM International
Published: 01 December 2006
DOI: 10.31399/asm.tb.cw.t51820203
EISBN: 978-1-62708-339-3
... corrosion of weldments are used to assess intergranular corrosion of stainless steels and high-nickel alloys. Other applicable tests evaluate pitting and crevice corrosion, stress-corrosion cracking, and microbiologically influenced corrosion. Each of these test methods is reviewed in this chapter...
Abstract
This chapter addresses in-service monitoring and corrosion testing of weldments. Three categories of corrosion monitoring are discussed: direct testing of coupons, electrochemical techniques, and nondestructive testing techniques. The majority of the test methods for evaluating corrosion of weldments are used to assess intergranular corrosion of stainless steels and high-nickel alloys. Other applicable tests evaluate pitting and crevice corrosion, stress-corrosion cracking, and microbiologically influenced corrosion. Each of these test methods is reviewed in this chapter.
Image
Published: 01 December 2008
Fig. 28 Stress corrosion cracking (SCC) in neutral aerated NaCl. Testing duration 1000 hr. Source: Ref 5
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Image
in Stress-Corrosion Cracking of Nickel-Base Alloys[1]
> Stress-Corrosion Cracking<subtitle>Materials Performance and Evaluation</subtitle>
Published: 01 January 2017
Fig. 5.13 Stress-corrosion cracking behavior of Hastelloy C-276 vs. testing temperature. Heat treatment: 260 °C (500 °F) for 250 h; environment: 25% NaCl + 0.5% CH 3 COOH + 1 g/L S 8 + H 2 S; yield strength: 1050 to 1160 MPa (152 to 168 ksi); stress level: 70 and 90% of yield strength. Source
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Image
in Stress-Corrosion Cracking of Magnesium Alloys[1]
> Stress-Corrosion Cracking<subtitle>Materials Performance and Evaluation</subtitle>
Published: 01 January 2017
Fig. 9.3 Stress-corrosion cracking in an extruded Mg-6Al-1Zn alloy tested in a salt-chromate solution, showing (a) intergranular crack propagation in the furnace-cooled alloy and (b) transgranular propagation in the water-quenched material. Source: Ref 9.26
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Image
Published: 01 November 2007
Fig. 14.4 Corrosion depth for unstressed and stressed specimens of alloy 800H tested at 800 °C (1470 °F) in H 2 -1.2H 2 O-0.4H 2 S (5 × 10 –22 atm p O 2 , 4×10 –9 atm p S 2 ). Also included was the data generated from H 2 -1.2H 2 O-7CO-0.4H 2 S (5 × 10 –22 atm p O 2 , 5 × 10 –9
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Image
Published: 01 November 2007
Fig. 14.9 Stress-assisted preferential corrosion penetration for alloy 45TM tested to 2% strain at 600 °C (1110 °F) for 1820 h in CO-32H 2 -4CO 2 -0.2H 2 S. Note: the tested specimen surface was plated prior to the mounting of the metallographic sample to retain the surface corrosion products
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Image
in Deformation and Fracture Mechanisms and Static Strength of Metals
> Mechanics and Mechanisms of Fracture: An Introduction
Published: 01 August 2005
Fig. 2.98 Stress-corrosion cracking in an extruded Mg-6Al-1Zn alloy tested in a salt-chromate solution. (a) Intergranular crack propagation in the face-cooled alloy. (b) Transgranular crack propagation in the water-quenched material. Source: Ref 2.72
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