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Published: 01 January 1996
Fig. 23 Effect of specimen thickness on the SCC susceptibility of titanium alloys. (a) Fracture toughness of duplex-annealed Ti-8Al-1Mo-1V and mill-annealed Ti-6Al-4V, tested in air and in 3.5% NaCl. (b) Variation of fracture toughness with specimen thickness. t crit , specimen thickness
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Published: 01 January 1997
Fig. 8 Effect of specimen thickness, loading rate, and temperature on fracture toughness. In general, increasing the specimen thickness will decrease the fracture toughness to a limiting (or critical) value. Additionally, increasing the temperature and decreasing the loading rate will shift
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Published: 01 January 1986
Fig. 90 STEM (a) and thickness profiles (b) for a NiAl/Ni specimen held at 1100 °C (2010 °F) for 15 min. The subscript ss denotes solid solution. Source: Ref 75
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in Failures of Pressure Vessels and Process Piping
> Analysis and Prevention of Component and Equipment Failures
Published: 30 August 2021
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Published: 01 January 2006
Fig. 8 Stretch-formed specimen. Material: MgAl3Zn1 (AZ31); initial sheet thickness, s 0 : 1.3 mm (0.051 in.); forming temperature: 250 °C (480 °F). Source: Ref 15
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Published: 01 January 1996
Fig. 22 Effects of loading rate, thickness, specimen dimensions, and crack depth on the ductile-to-brittle transition behavior
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Series: ASM Handbook
Volume: 8
Publisher: ASM International
Published: 01 January 2000
DOI: 10.31399/asm.hb.v08.a0003276
EISBN: 978-1-62708-176-4
... Abstract This article reviews the factors that have a significant effect on the selection and interpretation of results of different hardness tests, namely, Brinell, Rockwell, Vickers, and Knoop tests. The factors concerned include hardness level (and scale limitations), specimen thickness...
Abstract
This article reviews the factors that have a significant effect on the selection and interpretation of results of different hardness tests, namely, Brinell, Rockwell, Vickers, and Knoop tests. The factors concerned include hardness level (and scale limitations), specimen thickness, size and shape of the workpiece, specimen surface flatness and surface condition, and indent location. The article focuses on the selection for specific types of materials, such as steels, cast irons, nonferrous alloys, and plastics, and industrial applications, of hardness tests.
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Published: 01 January 2002
Fig. 13 Aluminum alloy fracture mechanics test specimen, 6.3 mm (0.25 in.) thick. Fatigue crack at left of arrows is flat and perpendicular to side surfaces (note absence of beach marks in this laboratory fatigue fracture). Overload fracture to right of arrows has 45° shear lips extending
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Published: 01 January 2002
Fig. 16 Crack arrest lines on edge-notched tension specimens. Material thickness 13 mm ( 1 2 in.), 10 mm ( 3 8 in.), and 6 mm ( 1 4 in.). Note the distance for first arrest, which increases with section thickness, and note that the arrest lines are not closed
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Published: 01 December 2004
Fig. 20 Aluminum alloy fracture mechanics test specimen, 6.3 mm (0.25 in.) thick. Fatigue crack at left of arrows is flat and perpendicular to side surfaces (note absence of beach marks in this laboratory fatigue fracture). Overload fracture to right of arrows has 45° shear lips extending
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Published: 01 November 1995
Fig. 48 Compressive relaxation of 30% GF PET. Specimen: 3.2 mm (0.13 in.) thick under aluminum washers with area of 172 mm 2 (0.266 in. 2 ). Temperature: 23 °C (73 °F). Initial stresses: 35 to 104 MPa (5 to 15 ksi)
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Published: 01 January 1993
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Published: 15 June 2019
Fig. 20 Sectioned specimens cut from 1.6 mm (0.064 in.) thick alloy 3003-H14 panels after exposure in two environments
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Published: 15 May 2022
Fig. 1 Activation spectra of 760 μm (30 mil) thick polycarbonate specimen using 6000 W xenon weatherometer with borosilicate filters plus short-wavelength cutoff filters. Source: Ref 3
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Published: 01 January 2001
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Published: 15 January 2021
Fig. 17 Crack-arrest lines on edge-notched tension specimens. Material thickness: 13 mm (½ in.), 10 mm (⅜ in.), and 6 mm (¼ in.). Note the distance for first arrest, which increases with section thickness, and note that the arrest lines are not closed along the centerline in the 13 mm
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Published: 15 January 2021
Fig. 13 Aluminum alloy fracture mechanics test specimen, 6.3 mm (0.25 in.) thick. Fatigue crack at left of arrows is flat and perpendicular to side surfaces (note absence of beach marks in this laboratory fatigue fracture). Overload fracture to right of arrows has 45° shear lips extending
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Published: 01 January 2001
Fig. 20 Thick adherend specimen for characterizing the shear properties of adhesives. Dimensions in inches
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Published: 01 January 1993
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in Directionally Solidified and Single-Crystal Superalloys
> Properties and Selection: Irons, Steels, and High-Performance Alloys
Published: 01 January 1990
Fig. 16 CMSX-4 (heat VF 719) SX test of flat specimen, 25 mm wide by 1.25 mm thick by 100 mm long (1 in. by 0.05 in. by 4 in.). Specimen was cast, 99% solutioned, and double aged. Micrographs taken from longitudinal orientation. (a) 90×. (b) 365×. (c) 905×. (d) 905×
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