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Series: ASM Technical Books
Publisher: ASM International
Published: 01 November 2019
DOI: 10.31399/asm.tb.mfadr7.t91110032
EISBN: 978-1-62708-247-1
... Abstract The management of a failure analysis (FA) laboratory requires a broad range of activities to optimize the efficiency of the operation. The purpose of this article is to stimulate readers to consider the various aspects of FA laboratory operations and their respective business...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 March 2002
DOI: 10.31399/asm.tb.mgppis.t60400087
EISBN: 978-1-62708-258-7
... Abstract This chapter discusses the important role of metallography and the metallographer in predicting and understanding the properties of metals and alloys. Examples are presented of a metallographer working as part of a team in a research laboratory of a large steel company...
Series: ASM Technical Books
Publisher: ASM International
Published: 01 March 2002
DOI: 10.31399/asm.tb.mgppis.t60400149
EISBN: 978-1-62708-258-7
... microscopes, x-ray diffractometers, microhardness testers, and hot microhardness testers. A list of other instruments that are usually located in a research laboratory or specialized testing laboratory is also provided. electron probe microanalyzers image analyzers metallographic laboratory...
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Published: 01 December 2006
Fig. 23 Scanning electron micrograph of the laboratory-induced fracture. Dimples are characteristic of microvoid coalescence, a ductile form of fracture. More
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Published: 30 April 2021
Fig. 3.20 Friction coefficient trends observed over 30 years of laboratory testing of many different tribocouples More
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Published: 01 August 2015
Fig. 12.6 Laboratory procedures for etching in induction heat treating. Source: Ref 6 More
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Published: 01 December 1999
Fig. 1.5 Internal oxidation of a Ni-Cr steel carburized in a laboratory furnace, showing both grain boundary oxides and oxide precipitates within grains. 550× More
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Published: 01 December 2003
Fig. 4 Laboratory abrasive cutoff device More
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Published: 01 November 2010
Fig. 2.11 Composite material that was subjected to a laboratory-induced lightning strike. The section shown is 1 mm (0.04 in.) away from the center of the strike. This sample was first impregnated with Rhodamine-B-dyed epoxy casting resin and then, after sectioning, mounted with Coumarin 35 More
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Published: 30 November 2013
Fig. 18 Typical fatigue ( S-N ) diagram of laboratory fatigue testing of medium-strength ferrous metal. More
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Published: 01 December 1989
Fig. 6.47. Results of laboratory solid-particle erosion tests ( Ref 114 and 115 ). Note: At end of 100-h test   • 80% of original plasma coating present   • <10% of original diffusion coating present More
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Published: 01 December 2003
Fig. 26 SEM view of fatigue striations in medium-density polyethylene, laboratory tested at 0.5 Hz with maximum stress 30% of the yield strength. Crack growth is upward in this view. Original magnification 200×. Source: Ref 23 More
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Published: 01 December 2015
Fig. 17 Results of laboratory tests conducted in synthetic flue gas (80N 2 -15CO 2 -4O 2 -1SO 2 , saturated with H 2 O) with synthetic ash (37.5 mol% Na 2 SO 4 , and 25 mol% Fe 2 O 3 ) covering samples. Exposure was 50 h. Source: Ref 5 More
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Published: 01 December 1984
Figure 2-2 Typical laboratory abrasive cutoff saw. (Courtesy of Buehler Ltd.) More
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Published: 01 November 2019
Fig 17 Line scans of unaged VCSELs, laboratory (“ALT”) aged VCSELs, and VCSELs with ❬100❭ DLDs. The line scans were taken from the devices shown in the previous figure, and oriented from the darkest to the lightest points. More
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Published: 01 December 2015
Fig. 22 Laboratory-simulated flue gas corrosion versus temperature for selected alloys. Tests were conducted in synthetic flue gas (80N 2 -15CO 2 -4O 2 -1SO 2 , saturated with water) with synthetic ash (37.5 mol % Na 2 SO 4 , 37.5 mol% K 2 SO 4 , 25 mol% Fe 2 O 3 ). Source: Ref 135 More
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Published: 01 October 2011
Fig. 7.23 Laboratory simulation of the multistage fatigue process More
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Published: 01 September 2008
Fig. 32 Laboratory simulation of adequate and inadequate heat treating conditions for AISI H13. The first situation (condition 1) is the recommended heat treatment: hardening at 1020 °C, followed by two tempering treatments at high temperature. In this case, 45 HRC was desired, and thus More
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Published: 01 September 2008
Fig. 22 SEM examination of the failed roll pin and laboratory-produced overload fractures. (a) Location A of the service failure (20 μm). (b) Location A of the service failure showing intergranular fracture with some dimples (5 μm). (c) Laboratory-produced overload failure showing More
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Published: 01 September 2008
Fig. 45 Dimpled rupture indicating overload failure in a laboratory-produced failure. Original magnification: 5000× More