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Book Chapter

By P.F. Timmins
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002386
EISBN: 978-1-62708-193-1
... an operating stress map based on the principles used in constructing a residual strength diagram. These include plane strain fracture toughness, net section yield, and empiricism. The article details the fatigue crack growth behavior based on stress-corrosion cracking rates and corrosion fatigue factor...
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002406
EISBN: 978-1-62708-193-1
... Abstract This article provides an overview of fatigue and fracture resistance of aluminum alloys. It discusses the characteristics of aluminum alloy classes and the fracture mechanics of aluminum alloys. The article tabulates relative stress-corrosion cracking ratings for high-strength wrought...
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Published: 01 December 1998
Fig. 12 Crack-growth rate curve for stress-corrosion cracking. (a) Idealized crack growth rate curve where regime I is SCC enhancement of cracking above the threshold. In regime II, mechanical enhancement has attained a maximum, and cracking is transport controlled. In regime III, the process More
Image
Published: 01 January 1996
Fig. 12 Crack growth rate curve for stress-corrosion cracking. (a) Idealized crack growth rate curve where regime I is SCC enhancement of cracking above the threshold. In regime II the mechanical enhancement has attained a maximum and cracking is transport controlled. In regime III the process More
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Published: 01 January 2003
Fig. 31 Stress-corrosion crack growth as a function of the two strain rate thresholds, ε ˙ 1 and ε ˙ 2 More
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Published: 01 January 2003
Fig. 37 Effects of beam deflection rate on stress-corrosion crack velocity in precracked cantilever bend specimens of a carbon-manganese steel. Tested in a carbonate-bicarbonate solution at 75 °C (165 °F) and at a potential of −650 mV versus SCE. Source: Ref 62 More
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Published: 15 June 2019
Fig. 7 Effect of strain rate on stress-corrosion cracking (SCC) and hydrogen-induced cracking. Source: Ref 28 More
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Published: 15 June 2019
Fig. 8 Strain-rate regimes for studying stress-corrosion cracking of various aluminum alloys. Corrodent: 3% sodium chloride plus 0.3% hydrogen peroxide. Source: Ref 29 More
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Published: 15 June 2019
Fig. 10 Crack propagation rates in stress-corrosion tests using precracked specimens of high-strength 2 xxx -series aluminum alloys, 25 mm (1 in.) thick, double-cantilever beam, transverse-longitudinal (short-longitudinal) orientation of plate, wet twice a day with an aqueous solution of 3.5 More
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Published: 15 June 2019
Fig. 12 Crack propagation rates in stress-corrosion tests using 7 xxx -series aluminum alloys, 25 mm (1 in.) thick, double-cantilever beam, short-transverse orientation of die, transverse orientation of die forgings and plate, alternate immersion tests, 23 °C (73 °F). Source: Ref 25 More
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Published: 15 June 2019
Fig. 13 Stress-corrosion crack propagation rates for various aluminum alloy 7050 products. Double-beam specimens (short-longitudinal) bolt-loaded to pop-in and wetted three times daily with 3.5% NaCl. Plateau velocity averaged over 15 days. The right end of the band for each product indicates More
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Published: 15 June 2019
Fig. 12 (a) Crack propagation rates in stress-corrosion tests using precracked thick, double-cantilever beam specimens of high-strength 2 xxx -series aluminum alloy plate, transverse-long (short-longitudinal) orientation. Specimens were wet twice a day with an aqueous solution of 3.5% NaCl, 23 More
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Published: 15 June 2019
Fig. 10 Stress-corrosion crack growth rates for (a) 2 xxx and (b) 7 xxx alloys in precracked short-transverse double-cantilever beam specimens as a function of applied stress-intensity factor. Source: Ref 13 More
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Published: 01 January 1996
Fig. 13 Crack propagation rates in stress corrosion tests using precracked specimens of high-strength 2XXX series aluminum alloys, 25 mm thick, double cantilever beam, TL(S-L) orientation of plate, wet twice a day with an aqueous solution of 3.5% NaCl, 23 °C More
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Published: 01 January 1996
Fig. 14 Crack propagation rates in stress corrosion tests using 7XXX series aluminum alloys, 25 mm thick, double cantilever beam, short-transverse orientation of die transverse orientation of die forgings and plate, alternate immersion tests, 23 °C. Source: M.O. Speidel, Met. Trans., Vol 6A More
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Published: 01 January 2005
Fig. 10 (a) Crack propagation rates in stress-corrosion tests using precracked thick, double-cantilever beam specimens of high-strength 2 xxx -series aluminum alloy plate, TL (SL) orientation. Specimens were wet twice a day with an aqueous solution of 3.5% NaCl, 23 °C (73 °F). (b) Crack More
Book Chapter

Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.a0003130
EISBN: 978-1-62708-199-3
... ratings can be used in industrial and seacoast atmospheres without protection. Alloys with C, D, and E ratings generally should be protected, at least on faying surfaces. (b) Stress-corrosion cracking ratings are based on service experience and on laboratory tests of specimens exposed to alternate...
Series: ASM Handbook
Volume: 2B
Publisher: ASM International
Published: 15 June 2019
DOI: 10.31399/asm.hb.v02b.a0006545
EISBN: 978-1-62708-210-5
... and Propagation Stress-corrosion cracking is a delayed failure process. That is, cracks initiate and propagate at a slow rate from 10 −6 to 10 −3 mm/s (4 × 10 −7 to 4 × 10 −4 in./s), until the stresses exceed the fracture strength. The process of SCC is usually discussed in terms of initiation...
Book Chapter

By R.H. Jones
Series: ASM Handbook
Volume: 13A
Publisher: ASM International
Published: 01 January 2003
DOI: 10.31399/asm.hb.v13a.a0003633
EISBN: 978-1-62708-182-5
... Hydride Aluminum alloys, steels Various media Near-surface hydrogen The Phenomenon of SCC Stress-corrosion cracking is a delayed failure process. That is, cracks initiate and propagate at a slow rate from 10 −9 to 10 −6 m/s (4 × 10 −7 to 4 × 10 −4 in./s), until the stresses...
Book Chapter

By P.S. Pao
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002361
EISBN: 978-1-62708-193-1
... fatigue conditions that under a static stress-corrosion cracking condition. Depending on the stress level and the cyclic frequency, the crack growth rates may be high under both stress-corrosion and corrosion fatigue. However the underlying mechanisms for both corrosion fatigue and stress-corrosion...