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notched specimen
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in Fatigue Resistance of Steels
> Properties and Selection: Irons, Steels, and High-Performance Alloys
Published: 01 January 1990
Fig. 30 Fatigue data (a) showing sequence effects for notched-specimen and smooth-specimen simulations (2024-T4 aluminum, K f = 2.0). Load histories A and B have a similar cyclic load pattern (Δ S 2 ) but have slightly different initial transients (Δ S 1 ) with either (b) a tensile
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Published: 01 January 2002
Fig. 22 Two views of a notched specimen that was electroplated with copper, wrapped with copper wire, and tested for 3 h at 1100 °C (2010 °F) without application of a load. No grain-boundary penetration of copper or intergranular cracking is evident, but there is evidence of minor bulk
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Image
Published: 01 January 2000
Fig. 1 Schematic illustration of an edge-notched specimen. (a) Crack length, a , and general coordinate system for crack tip stresses in Mode I loading.
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Published: 01 January 1996
Fig. 35 Fatigue data (a) showing sequence effects for notched-specimen and smooth-specimen simulations (2024-T4 aluminum, K f = 2.0). Load histories A and B have a similar cyclic load pattern (Δ S 2 ) but have slightly different initial transients (Δ S 1 ) with either (b) a tensile
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Published: 01 January 1990
Fig. 2 Charpy V-notch specimen used for the evaluation of notch toughness (ASTM E 23). Dimensions given in millimeters
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in Mechanisms and Appearances of Ductile and Brittle Fracture in Metals
> Failure Analysis and Prevention
Published: 01 January 2002
Fig. 65 Charpy V-notch specimen (notch area outlined) with crack path along shear plane due to crack-tip blunting
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Image
Published: 01 December 1998
Fig. 30 Charpy V-notch specimen used for the evaluation of notch toughness (ASTM E 23). Dimensions given in millimeters
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in Mechanisms and Appearances of Ductile and Brittle Fracture in Metals
> Failure Analysis and Prevention
Published: 15 January 2021
Fig. 65 Charpy V-notch specimen (notch area outlined) with crack path along shear plane due to crack-tip blunting
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Published: 01 January 1990
Fig. 5 Fracture surfaces of the broken Charpy V-notch specimens in Fig. 4 . These photographs show the amount of lateral expansion in nickel-chromium-molybdenum steel specimens tested in (a) the upper-shelf region (1.5 mm, or 0.059 mil) and (b) the lower-shelf region (0.05, or 0.002 mil
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Published: 01 January 1993
Fig. 11 Schematic showing location and orientation of Charpy V-notch specimens taken from the 1.07 m (42 in.) diameter X-65 steel pipe. Although inset shows widely spaced samples for the sake of clarity, actual samples removed are typically adjacent to one another.
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Published: 15 June 2019
Fig. 12 Rotating-beam ( R = −1.0) fatigue properties of notched specimens from wrought and cast aluminum alloys. Source: Ref 34
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Published: 01 January 1996
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Published: 01 December 1998
Fig. 26 Series of fractographs of Charpy V-notch specimens of 4340 steel tested at different temperatures, showing the change in appearance and estimated percentages of fibrous fracture. Source: Army Materials and Mechanics Research Center, Watertown Arsenal
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Book Chapter
Series: ASM Desk Editions
Publisher: ASM International
Published: 01 December 1998
DOI: 10.31399/asm.hb.mhde2.a0003243
EISBN: 978-1-62708-199-3
.... To determine the susceptibility of alloys to SCC and hydrogen embrittlement, several types of testing are available. This article describes the constant extension testing, constant load testing, constant strain-rate testing for smooth specimens and precracked or notched specimens of SCC. It provides...
Abstract
Stress-corrosion cracking (SCC) occurs under service conditions, which can result, often without any prior warning, in catastrophic failure. Hydrogen embrittlement is distinguished from stress-corrosion cracking generally by the interactions of the specimens with applied currents. To determine the susceptibility of alloys to SCC and hydrogen embrittlement, several types of testing are available. This article describes the constant extension testing, constant load testing, constant strain-rate testing for smooth specimens and precracked or notched specimens of SCC. It provides information on the cantilever beam test, wedge-opening load test, contoured double-cantilever beam test, three-point and four-point bend tests, rising step-load test, disk-pressure test, slow strain-rate tensile test, and potentiostatic slow strain-rate tensile test for hydrogen embrittlement.
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in Mechanisms and Appearances of Ductile and Brittle Fracture in Metals
> Failure Analysis and Prevention
Published: 01 January 2002
Fig. 18 Profile of fracture path in a notched-bar specimen taken from the long-transverse direction of HY-100 steel plate with a severely banded microstructure (alternating bands of ferrite and “granular” ferrite). Loading direction was perpendicular to the bands. Fracture is reported
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Published: 01 January 2000
Fig. 6 Gull-winging of single-edge notched-bar weld fracture toughness specimen. (a) Small scale of specimen that can be obtained from a longitudinal weld in a cylinder compared to full thickness. (b) Gull-winged specimen at full cylinder thickness ready to be loaded. Source: Ref 15
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Published: 01 January 2000
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Published: 01 January 2000
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Published: 01 January 2000
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Published: 01 January 2000
Fig. 19 Chevron notched beam (CNB) test specimen in three-point flexure for R -curve effects. Four normalized depth ratios (α o ) were included. Source: Ref 45
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