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Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.usage.c9001663
EISBN: 978-1-62708-236-5
... to ensure that personnel responsible for security and protection conduct themselves in a professional manner to minimize loss of property, personal injury, or loss of life in the event of an incident. Such exercises require that use of firearms be as close to authentic as possible; thus, M-16 automatic...
Series: ASM Failure Analysis Case Histories
Publisher: ASM International
Published: 01 June 2019
DOI: 10.31399/asm.fach.process.c0059924
EISBN: 978-1-62708-235-8
... forged into a doughnut preform in a large press, then formed into the ring by ring rolling. Fig. 1 Large rolled ring that was ultrasonically inspected as a 1.7 m (68 in.) diam billet and as a rolled ring A ring of this type requires a high degree of integrity; therefore, inspections were...
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Published: 15 January 2021
Fig. 38 Relation between initial period of metal-to-metal (M/M) contact and normal load. COF, coefficient of friction. Adapted from Ref 139 More
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Published: 15 January 2021
Fig. 54 High-cycle fatigue in D6AC steel at Δ K > 60 M P a m (54.6 ksi in .). (a) Macroscopic view of rapid fatigue growth under plane-stress conditions. (b) High-quality transmission electron microscopy replica showing elongated shear dimples from fatigue region More
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Published: 01 January 2002
Fig. 5 Surface of 1020 steel eroded by SiC at 80 m/s (260 ft/s) and 30° impact angle More
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Published: 01 January 2002
Fig. 14 Erosion rate of different metals and alloys (frequency = 20 kHz; specimen mounted in vibration horn; vibration amplitude = 50 μm; temperature = 20 °C; liquid: distilled water). Source: Ref 2 More
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Published: 01 January 2002
Fig. 22 Distortion in the web gap. M, bending moment; L, gap between surface of flange and weld to web More
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Published: 01 January 2002
Fig. 5 Subsurface fatigue origin in-service failure of 6.4 cm (2.5 in.) nitrided medium-carbon alloy steel crank pin. In contrast with the fracture surface shown in Fig. 4 , produced in the laboratory under continuous uniform loading, this surface exhibits beach marks. Courtesy of G.J. Fowler,... More
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Published: 01 January 2002
Fig. 6 High-cycle fatigue in D6AC steel at Δ K > 60 MPa m (54.6 ksi in. ). (a) Macroscopic view of rapid fatigue growth under plane-stress conditions. (b) High-quality TEM replica showing elongated shear dimples from fatigue region More
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Published: 01 January 2002
Fig. 3 Crack patterns of four specimens of MgF 2 broken in biaxial flexure. The more extensive branching is associated with higher stress at failure. Arrows indicate locations of fracture origins. Disks are ∼50 mm (2 in.) in diameter. Source: Ref 2 More
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Published: 01 January 2002
Fig. 39 Superimposed E -pH diagram of a 70Cu-30Zn alloy in 0.1 M NaCl. Lightly shaded area indicates the domain in which selective removal of zinc is expected in solutions free of copper ions. Intermediate shaded area indicates the domain in which both copper and zinc dissolves. Dark shaded More
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Published: 01 January 2002
Fig. 30 Correlation between evolution of M 6 C and Larson-Miller parameter for a 2 1 4 Cr-1Mo steel More
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Published: 01 January 2002
Fig. 34 Microstructure of Mar-M-247 heat treated cast alloy for gas turbine components showing different sizes of γ′ particles. Electropolished and electroetched. Courtesy of Dr. J.F. Radavich, Micro-Met Laboratories More
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Published: 01 January 2002
Fig. 10 Sign convention for shear ( V ) and bending moment ( M ) More
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Published: 01 January 2002
Fig. 40 Light micrograph showing wear damage at the surface of a 4485 alloy steel medart roll. The surface was nickel plated for edge retention and etched with nital. More
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Published: 01 January 2002
Fig. 47 Cyclic cleavage observations in Fe-4Ni (at.%) at 233 K, Δ K = 17 MPa m (15.5 ksi in. ). (a) Jogs formed during cyclic stepping across grain. (b) Large number of cleavage rivers formed to accommodate the twist angle misorientation between two grains. (c) Cleavage More
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Published: 01 January 2002
Fig. 53 High-cycle fatigue in D-6 AC steel at Δ K > 60 MPa m (54.6 ksi in. ). (a) Macroscopic view of rapid fatigue growth under plane-stress conditions. (b) High-quality TEM replica showing elongated shear dimples from fatigue region More
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Published: 01 January 2002
Fig. 10 Four tapered rings of locking device. Arrow indicates crack in one of the middle rings. More
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Published: 01 January 2002
Fig. 33 Typical workability behavior exhibited by different alloy systems. T M , absolute melting temperature. Source: Ref 17 More
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Published: 01 January 2002
Fig. 43 Incomplete fusion in a pulsed gas metal arc spot weld involving ERNiCu-7 (Monel 60), 0.89 mm (0.035 in.) diameter filler metal, copper-nickel to steel weldment. Etchant, 50% nitric-50% acetic acid. (a) View showing IF flaw. 30×. (b) View showing that IF was eliminated by tapering the ci... More