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Book: Fatigue and Fracture
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...
Abstract
This article describes the basis of operating stress maps based on failure assessment diagrams, which are used to assess potential fracture in the whole range of conditions from brittle to fully plastic behavior. It discusses the factors influencing the process of constructing 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. It summarizes the linear elastic fracture mechanics (LEFM) concepts for explaining the application of LEFM in damage tolerance analysis. The article exemplifies operating stress maps in a variety of applications.
Book Chapter
Selecting Aluminum Alloys to Resist Failure by Fracture Mechanisms
Available to PurchaseBook: Fatigue and Fracture
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...
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 aluminum products. It analyzes the selection of various alloys for stress-corrosion cracking resistance, including aluminum-lithium alloys, copper-free 7XXX alloys, and casting alloys. The article presents a list of typical tensile properties and fatigue limit of aluminum alloys. It also describes the effects of composition, microstructure, thermal treatments, and processing in fatigue crack growth of aluminum alloys.
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Crack-growth rate curve for stress-corrosion cracking. (a) Idealized crack ...
Available to PurchasePublished: 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
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Crack growth rate curve for stress-corrosion cracking. (a) Idealized crack ...
Available to PurchasePublished: 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
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Image
Stress-corrosion crack growth as a function of the two strain rate threshol...
Available to PurchasePublished: 01 January 2003
Fig. 31 Stress-corrosion crack growth as a function of the two strain rate thresholds, ε ˙ 1 and ε ˙ 2
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Effects of beam deflection rate on stress-corrosion crack velocity in precr...
Available to PurchasePublished: 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
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Effect of strain rate on stress-corrosion cracking (SCC) and hydrogen-induc...
Available to PurchasePublished: 15 June 2019
Fig. 7 Effect of strain rate on stress-corrosion cracking (SCC) and hydrogen-induced cracking. Source: Ref 28
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Strain-rate regimes for studying stress-corrosion cracking of various alumi...
Available to PurchasePublished: 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
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Crack propagation rates in stress-corrosion tests using precracked specimen...
Available to PurchasePublished: 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
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Crack propagation rates in stress-corrosion tests using 7 xxx -series alumi...
Available to PurchasePublished: 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
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Stress-corrosion crack propagation rates for various aluminum alloy 7050 pr...
Available to PurchasePublished: 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
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(a) Crack propagation rates in stress-corrosion tests using precracked thic...
Available to PurchasePublished: 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
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in Properties and Applications of Wrought Aluminum Alloys
> Properties and Selection of Aluminum Alloys
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
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Crack propagation rates in stress corrosion tests using precracked specimen...
Available to PurchasePublished: 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
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Crack propagation rates in stress corrosion tests using 7XXX series aluminu...
Available to PurchasePublished: 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
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(a) Crack propagation rates in stress-corrosion tests using precracked thic...
Available to PurchasePublished: 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
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Book Chapter
Corrosion Resistance of Aluminum and Aluminum Alloys
Available to PurchaseSeries: 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...
Abstract
This article discusses the corrosion resistance of aluminum and aluminum alloys in various environments, such as in natural atmospheres, fresh waters, seawater, and soils, and when exposed to chemicals and their solutions and foods. It describes the forms of corrosion of aluminum and aluminum alloys, including pitting corrosion, intergranular corrosion, exfoliation corrosion, galvanic corrosion, stray-current corrosion, deposition corrosion, crevice corrosion, filiform corrosion, stress-corrosion cracking, corrosion fatigue, and hydrogen embrittlement. The article also presents a short note on aluminum clad products and corrosion at joints.
Book Chapter
Stress-Corrosion Cracking of Aluminum Alloys
Available to PurchaseSeries: 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...
Abstract
In high-strength aluminum alloys, stress-corrosion cracking (SCC) is known to occur in ordinary atmospheres and aqueous environments. This article discusses the mechanisms of SCC in aluminum alloys, providing information on two main types of SCC models: those of anodic dissolution based on electrochemical theory and those that involve the stress-sorption theory of mechanical fracture. It reviews three different categories of experiments used to compare SCC performance of candidate materials for service. The categories are tests on statically loaded smooth samples, tests on statically loaded precracked samples, and tests using slowly straining samples. The article describes SCC susceptibility and ratings of SCC resistance for high-strength wrought aluminum products, such as 2xxx, 5xxx, and 7xxx series alloys, aluminum-lithium alloys, and 7xxx alloys containing copper.
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...
Abstract
Stress-corrosion cracking (SCC) is a phenomenon in which time-dependent crack growth occurs when the necessary electrochemical, mechanical, and metallurgical conditions exist. This article provides an overview of the environmental phenomenon, mechanisms, and controlling parameters of SCC. It describes the phenomenological and mechanistic aspects of the initiation and propagation of SCC. The article includes a phenomenological description of crack initiation and propagation that describes well-established experimental evidence and observations of stress corrosion. Discussions on mechanisms describe the physical process involved in crack initiation and propagation. The article also includes information on dissolution models and mechanical fracture models.
Book: Fatigue and Fracture
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...
Abstract
Corrosion fatigue refers to the phenomenon of cracking in materials under the combined actions of fatigue loading and a corrosive environment. This article focuses on the various mechanisms of corrosion fatigue, namely, hydrogen-assisted cracking, anodic dissolution, and surface energy reduction. It discusses the variables affecting corrosion fatigue. The effect of fatigue load frequency, environment, grain size, stress ratio, waveform, and temperature fatigue crack growth are also discussed.
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