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Eftink, Benjamin P.; Mara, Nathan Allan; Kingstedt, Owen T.; Safarik, Douglas Joseph
Los Alamos National Laboratory (LANL), Los Alamos, NM (United States). Funding organisation: USDOE National Nuclear Security Administration (NNSA) (United States); USDOE Office of Science - SC (United States)2017
Los Alamos National Laboratory (LANL), Los Alamos, NM (United States). Funding organisation: USDOE National Nuclear Security Administration (NNSA) (United States); USDOE Office of Science - SC (United States)2017
AbstractAbstract
[en] For this research, Split-Hopkinson pressure bar dynamic compression experiments were conducted to determine the defect/interface interaction dependence on interface type, bilayer thickness and interface orientation with respect to the loading direction in the Ag-Cu eutectic system. Specifically, the deformation microstructure in alloys with either a cube-on-cube orientation relationship with (111)Ag||(111)Cu interface habit planes or a twin orientation relationship with (3̄13)Ag||(1̄12)Cu interface habit planes and with bilayer thicknesses of 500 nm, 1.1 µm and 2.2 µm were probed using TEM. The deformation was carried by dislocation slip and in certain conditions, deformation twinning. The twinning response was dependent on loading orientation with respect to the interface plane, bilayer thickness, and interface type. Twinning was only observed when loading at orientations away from the growth direction and decreased in prevalence with decreasing bilayer thickness. Twinning in Cu was dependent on twinning partial dislocations being transmitted from Ag, which only occurred for cube-on-cube interfaces. Lastly, dislocation slip and deformation twin transfer across the interfaces is discussed in terms of the slip transfer conditions developed for grain boundaries in FCC alloys.
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Source
LA-UR--17-24245; OSTIID--1415383; AC52-06NA25396; FG52-09NA29463; Available from http://www.osti.gov/pages/biblio/1415383; DOE Accepted Manuscript full text, or the publishers Best Available Version will be available free of charge after the embargo period; Country of input: United States
Record Type
Journal Article
Journal
Materials Science and Engineering. A, Structural Materials: Properties, Microstructure and Processing; ISSN 0921-5093;
; v. 712; vp

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Shyam, Amit; Roy, Shibayan; Shin, Dongwon; Poplawsky, Jonathan D.; Allard Jr, Lawrence
Oak Ridge National Laboratory (ORNL), Oak Ridge, TN (United States). Funding organisation: USDOE Office of Energy Efficiency and Renewable Energy (EERE), Vehicle Technologies Office (EE-3V) (United States); USDOE Office of Science - SC, Basic Energy Sciences (BES). Scientific User Facilities Division (United States); USDOE Office of Science - SC, Basic Energy Sciences (BES) (SC-22). Materials Sciences & Engineering Division (United States)2019
Oak Ridge National Laboratory (ORNL), Oak Ridge, TN (United States). Funding organisation: USDOE Office of Energy Efficiency and Renewable Energy (EERE), Vehicle Technologies Office (EE-3V) (United States); USDOE Office of Science - SC, Basic Energy Sciences (BES). Scientific User Facilities Division (United States); USDOE Office of Science - SC, Basic Energy Sciences (BES) (SC-22). Materials Sciences & Engineering Division (United States)2019
AbstractAbstract
[en] Commonly used commercial cast aluminum alloys for the automotive industry are viable for temperatures only up to 250 °C, despite decades of study and development. Affordable cast aluminum alloys with improved high-temperature mechanical properties are needed to enable the next generation of higher efficiency passenger car engines. Metastable θ' (Al2Cu) precipitates contribute to strengthening in Al–Cu alloys, but above 250 °C coarsen and transform, leading to poor mechanical properties. A major challenge has been to inhibit coarsening and transformation by stabilizing the metastable precipitates to higher temperatures. In this work, we report compositions and associated counter-intuitive microstructures that allow cast Al–Cu alloys to retain their strength after lengthy exposures up to 350 °C, ~70% of their absolute melting point. Atomic-scale characterization along with first-principles calculations demonstrate that microalloying with Mn and Zr (while simultaneously limiting Si to < 0.1 wt %) is key to stabilization of high-energy interfaces. Lastly, it is suggested that segregation of Mn and Zr to the θ' precipitate-matrix interfaces provides the mechanism by which the precipitates are stabilized to a higher homologous temperature.
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OSTIID--1558572; AC05-00OR22725; Available from https://www.osti.gov/servlets/purl/1558572; DOE Accepted Manuscript full text, or the publishers Best Available Version will be available free of charge after the embargo period; arXiv:1902.08579
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Journal Article
Journal
Materials Science and Engineering. A, Structural Materials: Properties, Microstructure and Processing; ISSN 0921-5093;
; v. 765; vp

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Tamura, N.; Kunz, M.; Chen, K.; Celestre, R.S.; MacDowell, A.A.; Warwick, T.
Ernest Orlando Lawrence Berkeley National Laboratory, Berkeley, CA (United States). Funding organisation: Advanced Light Source Division (United States)2009
Ernest Orlando Lawrence Berkeley National Laboratory, Berkeley, CA (United States). Funding organisation: Advanced Light Source Division (United States)2009
AbstractAbstract
[en] Beamline 12.3.2 at the Advanced Light Source is a newly commissioned beamline dedicated to x-ray microdiffraction. It operates in both monochromatic and polychromatic radiation mode. The facility uses a superconducting bending magnet source to deliver an X-ray spectrum ranging from 5 to 22 keV. The beam is focused down to ∼ 1 um size at the sample position using a pair of elliptically bent Kirkpatrick-Baez mirrors enclosed in a vacuum box. The sample placed on high precision stages can be raster-scanned under the microbeam while a diffraction pattern is taken at each step. The arrays of diffraction patterns are then analyzed to derive distribution maps of phases, strain/stress and/or plastic deformation inside the sample.
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Source
LBNL--1807E; AC02-05CH11231; Available from OSTI as DE00953690; PURL: https://www.osti.gov/servlets/purl/953690-RCC4dp/
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Journal Article
Journal
Materials Science and Engineering. A, Structural Materials: Properties, Microstructure and Processing; ISSN 0921-5093;
; (Issue Jan 2009); vp

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Garlea, E.; Choo, H.; Sluss, C. C.; Koehler, M. R.; Bridges, R. L.
Brookhaven National Laboratory (BNL), Upton, NY (United States); Argonne National Laboratory (ANL), Argonne, IL (United States). Funding organisation: USDOE Office of Science - SC, Basic Energy Sciences (BES) (United States)2019
Brookhaven National Laboratory (BNL), Upton, NY (United States); Argonne National Laboratory (ANL), Argonne, IL (United States). Funding organisation: USDOE Office of Science - SC, Basic Energy Sciences (BES) (United States)2019
AbstractAbstract
[en] Elastic mechanical properties of 316 L stainless steel samples fabricated using laser powder bed fusion were studied non-destructively through resonant ultrasound spectroscopy. Samples in five different conditions were obtained by varying the laser power from 103 W (the highest density condition) to 68 W (the lowest density condition) at constant laser speed, producing samples with a volume energy density in the 24.5-16.5 J/mm(3) range and volumetric porosity in the 0.1-10% range. The observed elastic mechanical properties are discussed taking into consideration the bulk texture developed and quantitative pore characteristics studied using high-energy high-resolution synchrotron X-ray diffraction and X-ray computed micro-tomography, respectively. Furthermore, empirical exponential relationships are provided to express the functional dependence of Young's and shear moduli with porosity.
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OSTIID--1570662; SC0012704; AC02-06CH11357; Available from https://www.osti.gov/servlets/purl/1570662; DOE Accepted Manuscript full text, or the publishers Best Available Version will be available free of charge after the embargo period; Country of input: United States
Record Type
Journal Article
Journal
Materials Science and Engineering. A, Structural Materials: Properties, Microstructure and Processing; ISSN 0921-5093;
; v. 763(C); vp

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ALLOYS, AUSTENITIC STEELS, CARBON ADDITIONS, CHROMIUM ALLOYS, CHROMIUM STEELS, CHROMIUM-MOLYBDENUM STEELS, CHROMIUM-NICKEL STEELS, CHROMIUM-NICKEL-MOLYBDENUM STEELS, COHERENT SCATTERING, CORROSION RESISTANT ALLOYS, DIFFRACTION, HEAT RESISTANT MATERIALS, HEAT RESISTING ALLOYS, HIGH ALLOY STEELS, IRON ALLOYS, IRON BASE ALLOYS, LOW CARBON-HIGH ALLOY STEELS, MATERIALS, MECHANICAL PROPERTIES, MOLYBDENUM ALLOYS, NICKEL ALLOYS, SCATTERING, STAINLESS STEELS, STEEL-CR17NI12MO3-L, STEELS, TRANSITION ELEMENT ALLOYS
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Smith, Thale R.; Schoenung, Julie M.; San Marchi, Chris
Sandia National Laboratory (SNL-CA), Livermore, CA (United States). Funding organisation: USDOE National Nuclear Security Administration (NNSA) (United States)2019
Sandia National Laboratory (SNL-CA), Livermore, CA (United States). Funding organisation: USDOE National Nuclear Security Administration (NNSA) (United States)2019
AbstractAbstract
[en] Tensile properties, fatigue crack initiation, fatigue crack growth rate, and fatigue life are evaluated in 304L austenitic stainless steel fabricated by directed energy deposition (DED). Large lack of fusion (LoF) defects (often >1 mm in length) significantly reduce ultimate tensile strength and ductility, as well as accelerate fatigue crack initiation and reduce fatigue life. In comparison, small spherical defects (<100 μm in diameter) have less effect on tensile and fatigue properties. Fatigue crack growth rate is less severely affected by defects than other properties, showing only local acceleration in the proximity of LoF defects. Therefore, shorter fatigue life is attributed to the role of LoF defects on facilitating fatigue crack initiation and to a lesser extent fatigue crack propagation. Additionally, the fatigue life can be normalized for defects by considering their effect on ultimate tensile strength, suggesting that in the limit of low defect population, the fatigue strength of additively manufactured stainless steel is similar to conventional wrought materials.
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OSTIID--1570260; AC04-94AL85000; Available from https://www.osti.gov/servlets/purl/1570260; DOE Accepted Manuscript full text, or the publishers Best Available Version will be available free of charge after the embargo period; Country of input: United States
Record Type
Journal Article
Journal
Materials Science and Engineering. A, Structural Materials: Properties, Microstructure and Processing; ISSN 0921-5093;
; v. 765(C); vp

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External URLExternal URL
Zheng, B.; Haley, J. C.; Yang, N.; Yee, J.; Terrassa, K. W.
Sandia National Laboratory (SNL-CA), Livermore, CA (United States). Funding organisation: USDOE National Nuclear Security Administration (NNSA) (United States)2019
Sandia National Laboratory (SNL-CA), Livermore, CA (United States). Funding organisation: USDOE National Nuclear Security Administration (NNSA) (United States)2019
AbstractAbstract
[en] To identify the critical issues that affect the evolution of microstructure during additive manufacturing, we investigated the influence of process parameters on the evolution of the dimensional and surface quality, microstructure, internal defects, and mechanical properties in 316L stainless steel (SS) components fabricated using laser engineered net shaping (LENS®), a directed energy deposition (DED) additive manufacturing (AM) technique. The results show that the accumulation of un-melted powder particles on the side walls of deposited sections can be avoided by selecting a laser under-focused condition. Moreover, we report that the variation of melt pool width is more sensitive to laser power than to the depth of the melt pool. The formation of a so-called “hierarchical” microstructure with cellular morphology is attributable to a combination of layer deposition and rapid solidification, which are characteristics of AM. Finally, we discuss microstructure evolution and defect formation, particularly the formation of multiple interfaces and the presence of un-melted powder particles and pores, in light of the dynamic convective fluid flow and rapid solidification that occur in the melt pool. X-ray computed tomography (X-CT) was used to precisely map the spatial distribution of pores in the DED components. The evolution of microstructure during DED is discussed in the context of related thermal phenomena in an effort to provide fundamental insight into the mechanisms that govern defect formation.
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Source
OSTIID--1559510; AC04-94AL85000; NA0003525; Available from https://www.osti.gov/servlets/purl/1559510; DOE Accepted Manuscript full text, or the publishers Best Available Version will be available free of charge after the embargo period; Country of input: United States
Record Type
Journal Article
Journal
Materials Science and Engineering. A, Structural Materials: Properties, Microstructure and Processing; ISSN 0921-5093;
; v. 764(C); vp

Country of publication
ABSORPTION, ALLOYS, AUSTENITIC STEELS, CARBON ADDITIONS, CHROMIUM ALLOYS, CHROMIUM STEELS, CHROMIUM-MOLYBDENUM STEELS, CHROMIUM-NICKEL STEELS, CHROMIUM-NICKEL-MOLYBDENUM STEELS, CORROSION RESISTANT ALLOYS, DIAGNOSTIC TECHNIQUES, DISTRIBUTION, ELECTROMAGNETIC RADIATION, HEAT RESISTANT MATERIALS, HEAT RESISTING ALLOYS, HIGH ALLOY STEELS, IONIZING RADIATIONS, IRON ALLOYS, IRON BASE ALLOYS, LOSSES, LOW CARBON-HIGH ALLOY STEELS, MATERIALS, MOLYBDENUM ALLOYS, NICKEL ALLOYS, RADIATIONS, SORPTION, STAINLESS STEELS, STEEL-CR17NI12MO3-L, STEELS, TOMOGRAPHY, TRANSITION ELEMENT ALLOYS
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AbstractAbstract
[en] Low-cycle fatigue tests on cast nickel-based superalloy IN-100 were conducted at 10000C in air using sawtooth strain cycles over a wide range of frequencies (4x10-3-2 Hz) and tensile strain hold time tests. The influence of environment was investigated using tests under vacuum at the same temperature. The low cycle fatigue life was found to be strongly frequency dependent between 5x10-2 and 1 Hz. Testing in vacuum results in a much longer fatigue life than in air except for the higher test frequency. Crack growth rate data were measured using the potential drop technique and were used to show that the fatigue life in air is dominated by crack growth and to assess the influence of oxidation effects. (orig.)
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Journal Article
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Materials Science and Engineering. A, Structural Materials: Properties, Microstructure and Processing; ISSN 0921-5093;
; v. 101 p. 55-63

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ALLOYS, ALUMINIUM ALLOYS, BORON ADDITIONS, CARBON ADDITIONS, CHEMICAL REACTIONS, CHROMIUM ALLOYS, COBALT ALLOYS, COPPER ADDITIONS, CORROSION, CORROSION RESISTANT ALLOYS, FLUIDS, GASES, HEAT RESISTING ALLOYS, INCONEL ALLOYS, IRON ADDITIONS, MECHANICAL PROPERTIES, MOLYBDENUM ALLOYS, NICKEL ALLOYS, NICKEL BASE ALLOYS, TITANIUM ALLOYS, VANADIUM ADDITIONS, ZIRCONIUM ADDITIONS
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Yu, Chia-Chi; Chu, Jinn P.; Jia, Haoling; Shen, Yu-Lin; Gao, Yanfei
University of Tennessee, Knoxville, TN (United States); National Taiwan University of Science and Technology, Taipei, Taiwan (China). Funding organisation: USDOE Office of Science - SC, Basic Energy Sciences (BES) (SC-22) (United States); USDOE Office of Fossil Energy - FE (United States); US Army Research Office (ARO) (United States); National Science Foundation (NSF) (United States); Ministry of Science and Technology of Taiwan (China)2017
University of Tennessee, Knoxville, TN (United States); National Taiwan University of Science and Technology, Taipei, Taiwan (China). Funding organisation: USDOE Office of Science - SC, Basic Energy Sciences (BES) (SC-22) (United States); USDOE Office of Fossil Energy - FE (United States); US Army Research Office (ARO) (United States); National Science Foundation (NSF) (United States); Ministry of Science and Technology of Taiwan (China)2017
AbstractAbstract
[en] In this paper, a coating of the Zr-based thin-film metallic glass (TFMG) was deposited on the Zr50Cu30Al10Ni10 bulk metallic glass (BMG) to investigate shear-band evolution under four-point-bend fatigue testing. The fatigue endurance-limit of the TFMG-coated samples is ~ 33% higher than that of the BMG. The results of finite-element modeling (FEM) revealed a delay in the shear-band nucleation and propagation in TFMG-coated samples under applied cyclic-loading. The FEM study of spherical indentation showed that the redistribution of stress by the TFMG coating prevents localized shear-banding in the BMG substrate. Finally, the enhanced fatigue characteristics of the BMG substrates can be attributed to the TFMG coatings retarding shear-band initiation at defects on the surface of the BMG.
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Source
OSTIID--1360085; FE0008855; FE0024054; FE0011194; W911NF-13-1-0438; CMMI-1100080; DMR-1611180; 104-2218-E-011-018; Available from http://www.osti.gov/pages/biblio/1360085; DOE Accepted Manuscript full text, or the publishers Best Available Version will be available free of charge after the embargo period; Country of input: United States
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Journal Article
Journal
Materials Science and Engineering. A, Structural Materials: Properties, Microstructure and Processing; ISSN 0921-5093;
; v. 692; p. 146-155

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Nelaturu, Phalgun; Jana, Saumyadeep; Mishra, Rajiv S.; Grant, Glenn; Carlson, Blair E.
Pacific Northwest National Laboratory (PNNL), Richland, WA (United States). Funding organisation: USDOE (United States)2018
Pacific Northwest National Laboratory (PNNL), Richland, WA (United States). Funding organisation: USDOE (United States)2018
AbstractAbstract
[en] Here, failure by fatigue is a common problem associated with cast aluminum alloys due to defects like shrinkage porosities, non-metallic inclusions, etc. Friction stir processing (FSP) has recently emerged as an effective technique for local modification of microstructure. This study investigates the fatigue crack initiation and growth mechanisms in cast and FSPed A356 aluminum alloy. Two sets of parameters were used to friction stir the cast alloy resulting in the complete modification the cast microstructure to a wrought microstructure. Both the FSPed microstructures exhibited severe abnormal grain growth (AGG) after heat treatment leading to a multimodal grain size distribution – the grain sizes ranging from a few microns to a few millimeters. One of the FSP conditions displayed an excellent improvement in fatigue life by an order of magnitude, while the other condition displayed an unexpectedly large scatter in fatigue lives. Detailed study of the fractured fatigue specimens by electron back scattered diffraction (EBSD) revealed that both, fatigue crack initiation and propagation, were intimately tied to the grain size as well as the grain misorientations in the microstructure.
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Source
PNNL-SA--130375; OSTIID--1418022; AC05-76RL01830; Available from https://www.osti.gov/pages/biblio/1418022; DOE Accepted Manuscript full text, or the publishers Best Available Version will be available free of charge after the embargo period; Country of input: United States
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Journal Article
Journal
Materials Science and Engineering. A, Structural Materials: Properties, Microstructure and Processing; ISSN 0921-5093;
; v. 716; p. 165-178

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AbstractAbstract
[en] Low cycle fatigue tests on cast nickel-based superalloy IN-100 were conducted at various temperatures from 20 to 10000C in air under continuous-strain cycling at a constant total strain rate. The fatigue life was found to decrease with increasing temperature for a given total strain range. Fatigue cracks are partly crystallographic at low temperatures and strongly oxidized at high temperatures. The reduction in fatigue life is discussed using potential drop measurements and observations on interrupted test specimens. Testing at 10000C is shown to reduce drastically the crack initiation period and this behaviour is attributed to oxidation. (orig.)
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Journal Article
Journal
Materials Science and Engineering. A, Structural Materials: Properties, Microstructure and Processing; ISSN 0921-5093;
; v. 101 p. 47-54

Country of publication
ALLOYS, ALUMINIUM ALLOYS, BORON ADDITIONS, CARBON ADDITIONS, CHEMICAL REACTIONS, CHROMIUM ALLOYS, COBALT ALLOYS, COPPER ADDITIONS, CORROSION RESISTANT ALLOYS, CRYSTAL STRUCTURE, DIAGRAMS, FAILURES, FLUIDS, GASES, HEAT RESISTING ALLOYS, INCONEL ALLOYS, INFORMATION, IRON ADDITIONS, MECHANICAL PROPERTIES, MOLYBDENUM ALLOYS, NICKEL ALLOYS, NICKEL BASE ALLOYS, TITANIUM ALLOYS, VANADIUM ADDITIONS, ZIRCONIUM ADDITIONS
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