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Image
Published: 01 January 1986
Fig. 13 A second-order polynomial fit of intensity versus concentration
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Reversed-phase chromatogram of the product of the second step of the synthe...
Available to PurchasePublished: 01 January 1986
Fig. 14 Reversed-phase chromatogram of the product of the second step of the synthesis.
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Image
Comparison of dark-field light microscope fractograph (a) and an SEM second...
Available to PurchasePublished: 01 January 1987
Fig. 1 Comparison of dark-field light microscope fractograph (a) and an SEM secondary electron image (b) of the same area in an iron-chromium-aluminum alloy. Both 50×
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A second set of views, again at higher magnification, showing a fourth area...
Available to PurchasePublished: 01 January 1987
Fig. 15, 16 A second set of views, again at higher magnification, showing a fourth area of the surface of the low-cycle fatigue test fracture in aluminum alloy 7075-T6 in Fig. 13, 14 . This region of the fracture surface shows portions of two fatigue patches separated by a sizable step
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Image
A second set of views at higher magnification showing another area of the s...
Available to PurchasePublished: 01 January 1987
Fig. 19, 20 A second set of views at higher magnification showing another area of the stress-corrosion cracking fracture in aluminum alloy 7075-T6 in Fig. 17, 18 . Similar to the preceding set, this set of views shows a variety of grain surfaces resulting from intergranular rupture. The TEM
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Image
Published: 01 January 1987
Fig. 1227 TEM p-c replica at a second area of the facet at the arrow in Fig. 1225 , showing features resulting from transgranular cleavage and cleavage steps that cross a tilt boundary extending from lower right to upper left. The approximate direction of crack propagation was from lower left
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Image
Segment of a fractured second-stage gas-turbine wheel, cast from alloy 713C...
Available to PurchasePublished: 01 January 1987
Fig. 835 Segment of a fractured second-stage gas-turbine wheel, cast from alloy 713C, that broke from fatigue in service. (About half of the disk portion of the wheel was never recovered.) The fracture origin (at arrow) was in a grinding-relief groove adjacent to the wheel-balancing pad
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Image
Second fixture used by Lodge to simulate spalling. Courtesy of J.E. McGarry...
Available to PurchasePublished: 01 January 2002
Fig. 3 Second fixture used by Lodge to simulate spalling. Courtesy of J.E. McGarry
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Heat-damaged turbine blades. (a) Heat-damaged first- or second-stage turbin...
Available to Purchase
in Elevated-Temperature Life Assessment for Turbine Components, Piping, and Tubing
> Failure Analysis and Prevention
Published: 01 January 2002
Fig. 12 Heat-damaged turbine blades. (a) Heat-damaged first- or second-stage turbine blade (A), which remained intact but with a darkened appearance. It is common to have blades that appear to be in relatively good condition but with an underlying overtemperature condition. (b) Two third-stage
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Image
The DSC thermogram representing a second molding resin pellet that had prod...
Available to PurchasePublished: 01 January 2002
Fig. 21 The DSC thermogram representing a second molding resin pellet that had produced brittle parts. The thermogram shows a major melting transition associated with nylon 6/12 and a weaker transition attributed to nylon 6/6.
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A comparison of the second heating run results, further suggesting degradat...
Available to PurchasePublished: 01 January 2002
Fig. 24 A comparison of the second heating run results, further suggesting degradation of the failed sleeve material
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Second-phase cleavage fracture in Ti-6Al-4V. (a) Light micrograph of polish...
Available to PurchasePublished: 01 January 2002
Fig. 45 Second-phase cleavage fracture in Ti-6Al-4V. (a) Light micrograph of polished and etched surface. (b) SEM of fracture surface. Source: Ref 10
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Image
in Mechanisms and Appearances of Ductile and Brittle Fracture in Metals
> Failure Analysis and Prevention
Published: 01 January 2002
Fig. 22 Micrograph of specimen shown in Fig. 17 . Cleaved second-phase particles are visible in the microstructure, and no debonding at second-phase/matrix interfaces is visible. Source: Ref 42
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Image
The tip of the broken twistdrill. (a) End view. (b) Top view. A second dril...
Available to PurchasePublished: 01 January 2002
Fig. 2 The tip of the broken twistdrill. (a) End view. (b) Top view. A second drill from the same lot was also examined. There was carbide banding but to a significantly lesser degree. Hardness was measured as 63 to 64 HRC at both the flute edge and in the bulk of the drill.
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Tooling setup for external (first and second passes) and internal (third pa...
Available to PurchasePublished: 01 January 2005
Fig. 17 Tooling setup for external (first and second passes) and internal (third pass) upsetting of opposite ends of a steel tube. Dimensions given in inches
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Process sequence for upsetting a second head on a caster stem. Courtesy of ...
Available to PurchasePublished: 01 January 2005
Fig. 17 Process sequence for upsetting a second head on a caster stem. Courtesy of J. Bupp, National Machinery Co.
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Image
Published: 01 January 2005
Fig. 10 End-on view of the rail section being rolled in the second-from-last pass
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Published: 01 January 2006
Fig. 5 Effect of forming speed on ductility. fps, feet per second. Source: Ref 10
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