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Published: 01 January 1996
Fig. 5 Effect of specimen size on fatigue strength of magnesium alloys (smooth, rotating bending specimens). Source: Ref 6
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Published: 01 January 2002
Fig. 3 Illustration showing how depth of focus is dependent on specimen pixel size and aperture size
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Published: 15 January 2021
Fig. 3 Illustration showing how depth of focus is dependent on specimen pixel size and aperture size
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Published: 01 January 2000
Fig. 1 Tensile specimens having an initial grain size of 2.5 μm. Specimen A is untested. The other specimens were tested at 503 K and an initial strain rate of 1.33 × 10 −2 s −1 . Source: Ref 1
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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.a0002360
EISBN: 978-1-62708-193-1
... Abstract This article describes the fracture mechanics in fatigue. It discusses the fatigue crack growth rate (FCGR) testing that consists of several steps, beginning with selecting the specimen size, geometry, and crack length measurement technique. The two major aspects of FCGR test analysis...
Abstract
This article describes the fracture mechanics in fatigue. It discusses the fatigue crack growth rate (FCGR) testing that consists of several steps, beginning with selecting the specimen size, geometry, and crack length measurement technique. The two major aspects of FCGR test analysis are to ensure suitability of the test data and to calculate growth rates from the data. The article presents an analysis of the crack growth data. Optical, compliance, and electric potential difference are the most common laboratory techniques, and the article reviews their merits and limitations. Forced-displacement, forced-vibration, rotational-bending, resonance, and servomechanical systems for various loading conditions are also discussed.
Book: Fatigue and Fracture
Series: ASM Handbook
Volume: 19
Publisher: ASM International
Published: 01 January 1996
DOI: 10.31399/asm.hb.v19.a0002416
EISBN: 978-1-62708-193-1
... strength and tensile strength. The article reviews low velocity impacts in aircraft structures in terms of resin toughness, laminate thickness, specimen size and impactor mass, and post-impact fatigue. It explains the tension strength analysis, such as linear elastic fracture mechanics and R-curve methods...
Abstract
This article presents the damage tolerance criteria for military composite aircraft structures to safely operate the structures with initial defects or in-service damage. It describes the effects of defects, such as wrinkles in aircraft structures, and the reduction in compressive strength and tensile strength. The article reviews low velocity impacts in aircraft structures in terms of resin toughness, laminate thickness, specimen size and impactor mass, and post-impact fatigue. It explains the tension strength analysis, such as linear elastic fracture mechanics and R-curve methods, to predict the residual strength of the structures.
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Published: 01 August 2013
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Published: 01 December 1998
Fig. 5 Effect of section size on tensile strength of specimens cast from five classes of gray iron
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Published: 01 January 2000
Fig. 10 Location of standard tension-test specimen when turned from large sized fastener. Source: Ref 1
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Published: 01 December 1998
Fig. 28 Two sizes of the standard specimen for the Naval Research Laboratory standardized dynamic tear test. In the specimens, a crack with a sharp tip is produced by making a brittle electron beam weld or by pressing with a knife edge. With either method of providing the crack tip
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Image
Published: 01 January 1996
Fig. 42 Schematic relationship between grain size and (a) cylindrical specimens with a small surface crack and (b) thin standard C(T) specimens. Here the high density of grain boundaries hinders crack growth. (c) For thick standard C(T) specimens, this effect is overcompensated by roughness
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Published: 01 February 2024
Book Chapter
Series: ASM Handbook
Volume: 9
Publisher: ASM International
Published: 01 December 2004
DOI: 10.31399/asm.hb.v09.a0003786
EISBN: 978-1-62708-177-1
... Abstract Mounting of the specimen is often desirable or necessary for handling and metallographic polishing after the specimen is cut into an appropriate size. This article illustrates the different mechanical clamps used in mounting small specimens. It provides useful information...
Abstract
Mounting of the specimen is often desirable or necessary for handling and metallographic polishing after the specimen is cut into an appropriate size. This article illustrates the different mechanical clamps used in mounting small specimens. It provides useful information on compression molded mounts, which are molded with thermoplastic and thermosetting resins. The article reviews several resins and their key factors, which help in the selection of the most appropriate mounting method and resin. It also discusses the characteristics of plastic mounting materials. The article provides information on the molds and resins used for castable mounts, vacuum treatment of mounts, special mount arrangements, and mount marking and storage.
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Published: 01 January 1987
Fig. 6 Basic setups and lighting used to photograph fracture specimens and small parts. (a) General arrangement of camera, light source with diffuser, and specimen. Size and angle of the beam of light should be adjusted to give the best display of texture. A reflecting mirror or white card can
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Image
Published: 01 December 1998
Fig. 1 Basic setups and lighting used to photograph fracture specimens and small parts. (a) General arrangement of camera, light source with diffuser, and specimen. Size and angle of the beam of light should be adjusted to give the best display of texture. A reflecting mirror or white card can
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Published: 30 September 2014
Fig. 27 Effect of austenitizing temperature on relative volume change of different specimen sizes of 90MnV8 and 145CrV6 steels. Source: Ref 3
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Published: 01 January 1996
Fig. 14 Creep crack growth rate for 1Cr-1Mo- 1 4 V steels with differing specimen sizes. SG, side grooved. Source: Ref 51
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Published: 01 January 1996
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Published: 01 June 2016
Fig. 2 Variation of surface residual-stress magnitudes with increasing specimen size when cold water quenching ( T W < 20 °C, or 70 °F) rectilinear aluminum alloy blocks from 475 °C (890 °F). Multiple points from repeated experiments
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Published: 01 January 1990
Fig. 7 Dynamic tear energy versus temperature for as-cast and heat-treated ductile irons. Specimen size: 190 mm (7 1 2 in.) long, 130 mm (5 1 8 in.) wide, and 41 mm (1 5 8 in.) thick; 13 mm ( 1 2 in.) notch depth. Source: Ref 2
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