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Materials, Volume 14, Issue 11 (June-1 2021) – 444 articles

Cover Story (view full-size image): In the age of multidisciplinary frontiers in science and technology, glass stands as a pivotal material in many scientific and engineering cutting-edge applications. In the last few decades, inorganic glass was integrated into opto-electronic devices such as optical fibers, semiconductors, solar cells, transparent photovoltaic devices, or photonic crystals and in smart material applications such as environmental, pharmaceutical, and medical sensors, reinforcing its influence as an essential material and providing potential growth opportunities for the market. This paper presents and discusses examples of inorganic glasses in areas such as: (i) magnetic glass materials; (ii) solar cells and transparent photovoltaic devices; (iii) photonic crystal; (iv) smart materials. View this paper
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15 pages, 5873 KiB  
Article
Effect of SWCNT-Tuball Paper on the Lightning Strike Protection of CFRPs and Their Selected Mechanical Properties
by Kamil Dydek, Anna Boczkowska, Rafał Kozera, Paweł Durałek, Łukasz Sarniak, Małgorzata Wilk and Waldemar Łogin
Materials 2021, 14(11), 3140; https://doi.org/10.3390/ma14113140 - 7 Jun 2021
Cited by 12 | Viewed by 3763
Abstract
The main aim of this work was the investigation of the possibility of replacing the heavy metallic meshes applied onto the composite structure in airplanes for lightning strike protection with a thin film of Tuball single-wall carbon nanotubes in the form of ultra-light, [...] Read more.
The main aim of this work was the investigation of the possibility of replacing the heavy metallic meshes applied onto the composite structure in airplanes for lightning strike protection with a thin film of Tuball single-wall carbon nanotubes in the form of ultra-light, conductive paper. The Tuball paper studied contained 75 wt.% or 90 wt.% of carbon nanotubes and was applied on the top of carbon fibre reinforced polymer before fabrication of flat panels. First, the electrical conductivity, impact resistance and thermo-mechanical properties of modified laminates were measured and compared with the reference values. Then, flat panels with selected Tuball paper, expanded copper foil and reference panels were fabricated for lightning strike tests. The effectiveness of lightning strike protection was evaluated by using the ultrasonic phased-array technique. It was found that the introduction of Tuball paper on the laminates surface improved both the surface and the volume electrical conductivity by 8800% and 300%, respectively. The impact resistance was tested in two directions, perpendicular and parallel to the carbon fibres, and the values increased by 9.8% and 44%, respectively. The dynamic thermo-mechanical analysis showed higher stiffness and a slight increase in glass transition temperature of the modified laminates. Ultrasonic investigation after lightning strike tests showed that the effectiveness of Tuball paper is comparable to expanded copper foil. Full article
(This article belongs to the Special Issue Fabrication and Application of Electrically Conducting Composites)
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<p>Method of performing impact resistance tests, striking edge (<b>a</b>) perpendicular and (<b>b</b>) parallel to carbon fibres.</p>
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<p>Reference test panel (L_ref). Dimensions: 300 mm × 300 mm.</p>
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<p>Test panel with Tuball paper (L_TP). Dimensions: 300 mm × 300 mm.</p>
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<p>Test panel with ECF (L_ECF). Dimensions: 300 mm × 300 mm.</p>
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<p>View of the immersion method.</p>
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<p>Electrical conductivity of CFRP panels: (<b>a</b>) surface, (<b>b</b>) Z-direction (through the thickness).</p>
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<p>Microstructure of laminates cross-section: (<b>a</b>) L1, (<b>b</b>) L2, (<b>c</b>) L3. Arrows show the layer of Tuball paper.</p>
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<p>Microstructure of the cross-section of laminates with Tuball paper on the top: (<b>a</b>) and (<b>c</b>)—L2; (<b>b</b>) and (<b>d</b>)—L3. The arrow shows epoxy resin inside the layer.</p>
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<p>Impact resistance of analyzed laminates (<b>a</b>) perpendicular and (<b>b</b>) parallel to carbon fibres.</p>
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<p>Microstructure of laminates after impact tests: (<b>a</b>) L1, (<b>b</b>,<b>d</b>) L2, (<b>c</b>,<b>e</b>) L3.</p>
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<p>Storage modulus of reference (L1) and modified (L2, L3) laminates.</p>
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<p>Images of composites flat panels after a lightning strike (upper row) and ultrasonic C-Scan visualization (lower row) for: (<b>a</b>,<b>b</b>) L_ref, (<b>c</b>,<b>d</b>) L_TP and (<b>e</b>,<b>f</b>) L_ECF.</p>
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<p>Images of samples after a lightning strike and ultrasonic tests for (<b>a</b>) L_ref, (<b>b</b>) L_TP and (<b>c</b>) L_ECF, where C-Scan (top) and B-Scan (bottom) visualization.</p>
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25 pages, 29952 KiB  
Review
Degradation Mechanisms of Metal-Supported Solid Oxide Cells and Countermeasures: A Review
by Zhipeng Zhou, Venkata Karthik Nadimpalli, David Bue Pedersen and Vincenzo Esposito
Materials 2021, 14(11), 3139; https://doi.org/10.3390/ma14113139 - 7 Jun 2021
Cited by 21 | Viewed by 5813
Abstract
Metal-supported oxide cells (MSCs) are considered as the third-generation solid oxide cells (SOCs) succeeding electrolyte-supported (first generation) and anode-supported (second generation) cells, which have gained much attention and progress in the past decade. The use of metal supports and advanced technical methods (such [...] Read more.
Metal-supported oxide cells (MSCs) are considered as the third-generation solid oxide cells (SOCs) succeeding electrolyte-supported (first generation) and anode-supported (second generation) cells, which have gained much attention and progress in the past decade. The use of metal supports and advanced technical methods (such as infiltrated electrodes) has vastly improved cell performance, especially with its rapid startup ability and power density, showing a significant decrease in raw materials cost. However, new degradation mechanisms appeared, limiting the further improvement of the performance and lifetime. This review encapsulates the degradation mechanisms and countermeasures in the field of MSCs, reviewing the challenges and recommendations for future development. Full article
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<p>Schematic diagram of the structure and operating principle of SOFCs and SOECs. (<b>a</b>) SOFC mode with an oxide-conducting and proton-conducting electrolyte, respectively; (<b>b</b>) SOEC mode. An energy conversion efficiency of 50–60% can be achieved in SOFC mode [<a href="#B1-materials-14-03139" class="html-bibr">1</a>] and 90% in SOEC mode [<a href="#B8-materials-14-03139" class="html-bibr">8</a>].</p>
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<p>Schematic diagram of the development of SOFCs [<a href="#B9-materials-14-03139" class="html-bibr">9</a>,<a href="#B22-materials-14-03139" class="html-bibr">22</a>]. Note the thinner electrolyte allows a lower operating temperature, and the low operating temperature allows the use of metal supports.</p>
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<p>(<b>a</b>) Diagram of MSCs stack’s structure, reproduced with permission from Ref. [<a href="#B35-materials-14-03139" class="html-bibr">35</a>]; (<b>b</b>) 1 kW MSCs stack manufactured by Ceres Power, reproduced with permission from Ref. [<a href="#B36-materials-14-03139" class="html-bibr">36</a>].</p>
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<p>Two-dimensional slices from a spatially registered sub-dataset at identical locations in the electrode in the pristine (<b>a</b>), annealed for 3 h (<b>b</b>) and 8 h (<b>c</b>) states. Three different grey levels are present: black (pore), grey (YSZ), and white (nickel). (<b>d</b>) The nickel particle morphology at the same position before and after the annealing (in dry hydrogen at 850 °C). Reproduced with permission from Ref. [<a href="#B40-materials-14-03139" class="html-bibr">40</a>].</p>
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<p>(<b>a</b>) Operation of tubular metal-supported SOFCs at 700 °C with moist hydrogen fuel and oxygen as oxidant. Dashed line: as-infiltrated Ni anode, 300 m Acm<sup>−2</sup>; solid line: Ni anode was pre-coarsened at 800 °C, 100 mA cm<sup>−2</sup>, reproduced with permission from Ref. [<a href="#B23-materials-14-03139" class="html-bibr">23</a>]. (<b>b</b>) X-ray diffraction patterns for SDCN<sub>40</sub> anode catalyst upon reduction at 700 °C for 1 h (black) and after 100 h of thermal annealing at 700 °C in 3% humidified hydrogen (blue). (<b>c</b>) SDCN40 catalyst anode via thermal annealing at 700 °C and continuous electrochemical operation at 0.7 V for 100 h (corresponding to (<b>b</b>)). (<b>b</b>,<b>c</b>) are reproduced with permission from Ref. [<a href="#B52-materials-14-03139" class="html-bibr">52</a>].</p>
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<p>Schematic of the diffusion barrier layer method in metal-supported cells, reproduced with permission from Ref. [<a href="#B57-materials-14-03139" class="html-bibr">57</a>].</p>
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<p>(<b>a</b>) SEM image showing the polished cross-section of the planar metal-supported half-cell. The electrolyte is shown at the top, followed by the cermet layer and the metal support, reproduced with permission from Ref. [<a href="#B65-materials-14-03139" class="html-bibr">65</a>]. (<b>b</b>) Schematic diagram of the loss of conductivity of the metal support due to oxidation adapted from Ref. [<a href="#B9-materials-14-03139" class="html-bibr">9</a>]. (<b>c</b>) Cross-sectional SEM images of the metal support with a grown outer oxide layer in darker grey at different exposure times at 800 °C and 50%H<sub>2</sub>-50%H<sub>2</sub>O fuel atmospheres, reproduced with permission from Ref. [<a href="#B90-materials-14-03139" class="html-bibr">90</a>].</p>
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<p>SEM image of porous ITM support after La acetate coating with the. indication of area (<b>a</b>) thick and area (<b>b</b>) thin LaCrO<sub>3</sub>-coating, reproduced with permission from Ref. [<a href="#B95-materials-14-03139" class="html-bibr">95</a>].</p>
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<p>(<b>a</b>) Schematic representation of the mechanism of metal dusting corrosion of nickel, adapted from Ref. [<a href="#B43-materials-14-03139" class="html-bibr">43</a>]. (<b>b</b>) The interface between the Ni particle (lower part) and the YSZ electrolyte (upper part) close to the gas inlet area of the cell and (<b>c</b>) showing the carbon nanofibers and nanoparticles at the Ni-YSZ|YSZ interface, reproduced with permission from Ref. [<a href="#B96-materials-14-03139" class="html-bibr">96</a>].</p>
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<p>(<b>a</b>) Schematic diagram of the degradation mechanism caused by H<sub>2</sub>S poisoning reproduced with permission from Ref. [<a href="#B102-materials-14-03139" class="html-bibr">102</a>]. (<b>b</b>) Sulfur poisoning and regeneration or desulphurization processes of Ni-YSZ anodes in a fuel mixture with 50 ppm H<sub>2</sub>S, reproduced with permission from Ref. [<a href="#B101-materials-14-03139" class="html-bibr">101</a>].</p>
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<p>(<b>a</b>) Schematic illustration of the protonic ceramic fuel cell (PCFC) and mechanism of hydrocarbon reforming, water-gas shift reaction, sulfur cleaning, and carbon cleaning; (<b>b</b>) Mechanism of carbon cleaning. C<sub>ad</sub> indicates carbon absorbed on the surface of Ni. Reproduced with permission from Ref. [<a href="#B50-materials-14-03139" class="html-bibr">50</a>]. (<b>c</b>) Ionic conductivities of BZCYYb, BZCY, GDC, and YSZ measured at 400 to 750 °C in wet oxygen (with ~3 vol % H<sub>2</sub>O). (<b>d</b>) Typical current-voltage characteristics and the corresponding power densities measured at 750 °C for a cell with a configuration of Ni-BZCYYb|BZCYYb|BZCY-LSCF when ambient air was used as oxidant and hydrogen as fuel (with or without 20 ppm H<sub>2</sub>S contamination), and for another cell with a configuration of Ni-BZCYYb|SDC|LSCF when dry propane was used as fuel. Reproduced with permission from Ref. [<a href="#B51-materials-14-03139" class="html-bibr">51</a>]. Note BZY: BaZr<sub>0.9</sub>Y<sub>0.1</sub>O<sub>3−δ</sub>; BZCY: Ba(Zr<sub>0.1</sub>Ce<sub>0.7</sub>Y<sub>0.2</sub>)O<sub>3−δ</sub>; BZCYYb: BaZr<sub>0.1</sub>Ce<sub>0.7</sub>Y<sub>0.1</sub>Yb<sub>0.1</sub>O<sub>3−δ</sub>.</p>
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<p>Candidate materials for MSCs, adapted from Ref. [<a href="#B9-materials-14-03139" class="html-bibr">9</a>]. Lanthanum strontium manganite (LSM); Lanthanum nickel ferrite (LNF); Lanthanum strontium cobalt ferrite (LSCF); Strontium samarium cobaltite (SSC); Lanthanum Strontium Cobaltite (LSC); Scandia-ceria-stabilized zirconia (SCSZ); Lanthanum strontium gallium magnesium oxide (LSGM).</p>
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<p>(<b>a</b>) Structure diagram of the MSC with infiltrated electrodes. (<b>b</b>) SEM micrographs of the cross-section of the MSC showing the “metal-support/SCSZ backbone/SCSZ dense electrolyte/SCSZ backbone/metal-support” symmetric structure. (<b>c</b>) Cross-section of porous backbones and dense electrolyte. (<b>d</b>) Hydrogen electrode catalyst (Ni-SDC) infiltrated on SCSZ backbone (<b>e</b>) Oxygen electrode catalyst (Pr<sub>6</sub>O<sub>11</sub>) infiltrated on SCSZ backbone. Reproduced with permission from Ref. [<a href="#B118-materials-14-03139" class="html-bibr">118</a>].</p>
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<p>(<b>a</b>) Powder X-ray diffraction on PrOx cathode catalyst calcined at 600 °C (black) and after thermal annealing at 700 °C (blue) in the air for 100 h; (<b>b</b>) Impact of in situ catalyst pre-coarsening. MS-SOFC durability at 700 °C and 0.7 V before and after in situ catalyst pre-coarsening at 750 °C for 4 h; (<b>c</b>) Cr transport at the cathode side of a SOFC; (<b>d</b>) Bars represent quantified power retention (percentage of remaining power density after 100 h of operation vs. the beginning of life) observed for the post-sintering fabrication processes, individually and combined. Each process is associated with different colours and marking. Experimental results from whole cells are overlaid (blue stars). (<b>e</b>) Long-term durability for baseline and improved cell (after the cathode pre-coarsening, metal support pre-oxide, and ALD process) at 700 °C and 0.7 V. (<b>a</b>,<b>b</b>,<b>d</b>,<b>e</b>) were reproduced with permission from Ref. [<a href="#B52-materials-14-03139" class="html-bibr">52</a>]; (<b>c</b>) was adapted with permission from Ref. [<a href="#B116-materials-14-03139" class="html-bibr">116</a>].</p>
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<p>Images of TF-MSC. (<b>a</b>) structure diagram; (<b>b</b>) morphology and size; (<b>c</b>–<b>e</b>) Microstructure of the corresponding positions in (<b>a</b>). Reproduced with permission from Ref. [<a href="#B19-materials-14-03139" class="html-bibr">19</a>].</p>
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<p>(<b>A</b>). Low-tortuosity gas channels have higher gas diffusion efficiency, adapted from Ref. [<a href="#B81-materials-14-03139" class="html-bibr">81</a>]; (<b>B</b>). Gradient-porosity anodes facilitate electrochemical reactions, resulting in a higher power density, reproduced with permission from Ref. [<a href="#B152-materials-14-03139" class="html-bibr">152</a>]; (<b>C</b>). Regular-shaped and -distributed pores avoid the formation of small necks, increasing the lifetime of MSCs.</p>
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13 pages, 1896 KiB  
Article
Bio-Based Polyurethane Networks Derived from Liquefied Sawdust
by Kamila Gosz, Agnieszka Tercjak, Adam Olszewski, Józef Haponiuk and Łukasz Piszczyk
Materials 2021, 14(11), 3138; https://doi.org/10.3390/ma14113138 - 7 Jun 2021
Cited by 8 | Viewed by 2969
Abstract
The utilization of forestry waste resources in the production of polyurethane resins is a promising green alternative to the use of unsustainable resources. Liquefaction of wood-based biomass gives polyols with properties depending on the reagents used. In this article, the liquefaction of forestry [...] Read more.
The utilization of forestry waste resources in the production of polyurethane resins is a promising green alternative to the use of unsustainable resources. Liquefaction of wood-based biomass gives polyols with properties depending on the reagents used. In this article, the liquefaction of forestry wastes, including sawdust, in solvents such as glycerol and polyethylene glycol was investigated. The liquefaction process was carried out at temperatures of 120, 150, and 170 °C. The resulting bio-polyols were analyzed for process efficiency, hydroxyl number, water content, viscosity, and structural features using the Fourier transform infrared spectroscopy (FTIR). The optimum liquefaction temperature was 150 °C and the time of 6 h. Comprehensive analysis of polyol properties shows high biomass conversion and hydroxyl number in the range of 238–815 mg KOH/g. This may indicate that bio-polyols may be used as a potential substitute for petrochemical polyols. During polyurethane synthesis, materials with more than 80 wt% of bio-polyol were obtained. The materials were obtained by a one-step method by hot-pressing for 15 min at 100 °C and a pressure of 5 MPa with an NCO:OH ratio of 1:1 and 1.2:1. Dynamical-mechanical analysis (DMA) showed a high modulus of elasticity in the range of 62–839 MPa which depends on the reaction conditions. Full article
(This article belongs to the Section Biomaterials)
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<p>Changes in hydroxyl number depending on the liquefaction reaction temperature during heating.</p>
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<p>Water content in bio-polyols depending on the time of the liquefaction process.</p>
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<p>Bio-polyols flow curves.</p>
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<p>Bio-polyols viscosity curves.</p>
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<p>FTIR spectra of bio-polyols.</p>
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<p>The TGA and DTG curves of the polyurethane resins.</p>
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<p><span class="html-italic">Tan δ</span> and storage modulus (E′) of polyurethane resins.</p>
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14 pages, 2343 KiB  
Article
On the Rate of Interaction of Sodium Borohydride with Platinum (IV) Chloride Complexes in Alkaline Media
by Magdalena Luty-Błocho, Marek Wojnicki, Edit Csapo and Krzysztof Fitzner
Materials 2021, 14(11), 3137; https://doi.org/10.3390/ma14113137 - 7 Jun 2021
Cited by 6 | Viewed by 2909
Abstract
In this work, sodium borohydride was used as a strong reductant of traces of platinum complex ions. The investigations of the kinetics of redox reaction between platinum(IV) chloride complex ions and sodium borohydride were carried out. For the first time, the kinetic experiments [...] Read more.
In this work, sodium borohydride was used as a strong reductant of traces of platinum complex ions. The investigations of the kinetics of redox reaction between platinum(IV) chloride complex ions and sodium borohydride were carried out. For the first time, the kinetic experiments were carried out in a basic medium (pH~13), which prevents NaBH4 from decomposition and suppresses the release of hydrogen to the environment. The rate constants of Pt(IV) reduction to Pt(II) ions under different temperatures and concentrations of chloride ions conditions were determined. In alkaline solution (pH~13), the values of enthalpy and entropy of activation are 29.6 kJ/mol and –131 J/mol K. It was also found that oxygen dissolved in the solution strongly affects kinetics of the reduction process. Using collected results, the reduction mechanism was suggested. For the first time, the appearance of diborane as an intermediate product during Pt(IV) ions reduction was suggested. Moreover, the influence of oxygen present in the reacting solution on the rate of reduction reaction was also shown. Full article
(This article belongs to the Special Issue Research Progress on the Extractive Metallurgy)
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<p>(<b>a</b>) Spectrum of aqueous solutions containing 5ˑ10<sup>−4</sup> M Pt(IV) complex ions in 0.05 M NaOH; kinetic curve for Pt(IV) in 0.05 M NaOH registered at 262 nm (<b>a’</b>). Optical path length 2 mm; (<b>b</b>) change of absorption bands characteristic for Pt(IV) complex ions during the reaction with NaBH<sub>4</sub>. Conditions: C<sub>0,Pt(IV)</sub> = 0.05 mM, C<sub>0,NaBH4</sub> = 3.0 mM, I = 0.05 M, T = 50.0 ± 0.1 °C, pH = 12.9 ± 0.2, path length 1 cm.</p>
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<p>(<b>a</b>) Change of absorption bands characteristic for Pt(IV) complex ions during the reaction with NaBH<sub>4</sub>. Conditions: C<sub>0,Pt(IV)</sub> = 0.05 mM, C<sub>0,NaBH4</sub> = 3.0 mM, I = 0.05 M, T = 50.0 ± 0.1 °C, pH = 12.9 ± 0.2. Time of reaction 10 s (with step 0.2 s); (<b>b</b>) the change of absorbance value (A <math display="inline"><semantics> <mrow> <mo>∝</mo> <mo> </mo> </mrow> </semantics></math> concentration of Pt species) with time (kinetic curves) during the reaction of platinum ions with NaBH<sub>4</sub>. Conditions: C<sub>0,Pt(IV)</sub> = 0.05 mM, C<sub>0,NaBH4</sub> = 3.0 mM, I = 0.05 M, T = 50.0 ± 0.1 °C, pH = 12.9 ± 0.2, path length 1 cm.</p>
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<p>(<b>a</b>) The kinetic curves obtained at 262 nm for the reaction between platinum(IV) chloride complex ions and sodium borohydride in aqueous solution at different temperatures; (<b>b</b>) the sample of kinetic curve (change of Pt(IV) ions concentration in time of reaction reduction) at 25 °C (<b>b</b>). Conditions: C<sub>0,Pt(IV)</sub> = 0.05 mM, C<sub>0,NaBH4</sub> = 3.0 mM, pH = 12.9 ± 0.2.</p>
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<p>The linear plot of Eyring dependence (<span class="html-italic">T</span>·ln(<span class="html-italic">k</span><sub>1</sub>/<span class="html-italic">T</span>) vs. <span class="html-italic">T</span>) for the reaction between platinum(IV) chloride complex ions and sodium borohydride in aqueous solution. Conditions: C<sub>0,Pt(IV)</sub> = 0.05 mM, C<sub>0,NaBH4</sub> = 3.0 mM, pH = 12.9 ± 0.2.</p>
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<p>The influence of chloride ions addition on the observed rate constant for the reaction between platinum(IV) ions and sodium borohydride. Conditions: C<sub>0,Pt(IV)</sub> = 0.05 mM, C<sub>0,NaBH4</sub> = 3.0 mM, T = 25.0 ± 0.1 °C, pH = 12.9 ± 0.2.</p>
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<p>(<b>a</b>) Kinetic curves obtained for the reaction between platinum(IV) chloride complex ions and sodium borohydride at a standard procedure and in the case of deaerated solution; (<b>b</b>) kinetic curves registered in a short time. Conditions: C<sub>0,Pt(IV)</sub> = 0.05 mM, C<sub>0,NaBH4</sub> = 3.0 mM, T = 25.0 ± 0.1 °C, pH = 12.9 ± 0.2.</p>
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19 pages, 7917 KiB  
Article
Fatigue Behavior of Linear Friction Welded Ti-6Al-4V and Ti-6Al-2Sn-4Zr-2Mo-0.1Si Dissimilar Welds
by Sidharth Rajan, Priti Wanjara, Javad Gholipour and Abu Syed Kabir
Materials 2021, 14(11), 3136; https://doi.org/10.3390/ma14113136 - 7 Jun 2021
Cited by 6 | Viewed by 2566
Abstract
The use of joints fabricated from dissimilar titanium alloys allows the design of structures with local properties tailored to different service requirements. To develop welded structures for aerospace applications, particularly under critical loading, an understanding of the fatigue behavior is crucial, but remains [...] Read more.
The use of joints fabricated from dissimilar titanium alloys allows the design of structures with local properties tailored to different service requirements. To develop welded structures for aerospace applications, particularly under critical loading, an understanding of the fatigue behavior is crucial, but remains limited, especially for solid-state technologies such as linear friction welding (LFW). This paper presents the fatigue behavior of dissimilar titanium alloys, Ti–6Al–4V (Ti64) and Ti–6Al–2Sn–4Zr–2Mo–0.1Si (Ti6242), joined by LFW with the aim of characterizing the stress versus number of cycles to failure (S-N) curves in both the low- and high-cycle fatigue regimes. Prior to fatigue testing, metallurgical characterization of the dissimilar alloy welds indicated softening in the heat-affected zone due to the retention of metastable β, and the typical practice of stress relief annealing (SRA) for alleviating the residual stresses was effective also in transforming the metastable β to equilibrated levels of α + β phases and recovering the hardness. Thus, the dissimilar alloy joints were fatigue-tested in the SRA (750 °C for 2 h) condition and their low- and high-cycle fatigue behaviors were compared to those of the Ti64 and Ti6242 base metals (BMs). The low-cycle fatigue (LCF) behavior of the dissimilar Ti6242–Ti64 linear friction welds was characterized by relatively high maximum stress values (~ 900 to 1100 MPa) and, in the high-cycle fatigue (HCF) regime, the fatigue limit of 450 MPa at 107 cycles was just slightly higher than that of the Ti6242 BM (434 MPa) and the Ti64 BM (445 MPa). Fatigue failure of the dissimilar titanium alloy welds in the low-cycle and high-cycle regimes occurred, respectively, on the Ti64 and Ti6242 sides, roughly 3 ± 1 mm away from the weld center, and the transitioning was reasoned based on the microstructural characteristics of the BMs. Full article
(This article belongs to the Collection Welding and Joining Processes of Materials)
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<p>Bimodal microstructures of (<b>a</b>) Ti6242 and (<b>b</b>) Ti64 BMs.</p>
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<p>Schematics showing the (<b>a</b>) length (L), width (W) and depth (D) dimensions of the Ti64 BM and Ti6242 BM workpieces with the rolling direction (RD) and transverse direction (TD) orientations indicated; (<b>b</b>,<b>c</b>) Electro-discharge machining (EDM) plan for extracting the tensile, metallography and fatigue specimens from the welded coupons; (<b>d</b>) geometry of the tensile specimens; and (<b>e</b>) geometry of the fatigue specimens.</p>
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<p>Microhardness maps across the dissimilar Ti6242–Ti64 linear friction welds showing the weld line, weld center (WC), heat-affected zones (HAZs), thermomechanically affected zone (TMAZs), as well as the Ti6242 and Ti64 BMs: (<b>a</b>) as-welded (AWed) and (<b>b</b>) stress relief annealed (SRAed).</p>
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<p>Microstructural characteristics in the different regions of the dissimilar Ti6242–Ti64 linear friction welds in the (<b>a</b>–<b>c</b>) AWed condition and (<b>d</b>–<b>f</b>) SRAed condition.</p>
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<p>Microstructures in the WC at the weld line in the dissimilar Ti6242–Ti64 linear friction welds: (<b>a</b>) AWed condition and (<b>b</b>) SRAed condition.</p>
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<p>Average tensile properties of the AWed and SRAed dissimilar Ti6242–Ti64 welds.</p>
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<p>Secondary electron (SE) images of the tensile fracture surface for the (<b>a</b>,<b>b</b>) AWed and (<b>c</b>,<b>d</b>) SRAed conditions.</p>
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<p>Comparison of fatigue life curves at room temperature and R =  0.1 for the Ti6242 and Ti64 BMs relative to the dissimilar Ti6242–Ti64 linear friction weld in the SRAed condition: (<b>a</b>) semi-log scale plot of the maximum stress versus the number of cycles to failure (N<sub>f</sub>) in the (low cycle fatigue) LCF and high cycle fatigue (HCF) regimes and (<b>b</b>) double log scale plot of the maximum stress versus the number of reversals to failure (2Nf).</p>
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<p>Fatigue fracture surface: (<b>a</b>,<b>b</b>) LCF overview image with the arrow indicating the failure initiation site and higher -magnification image showing the predominant tensile overload region (Ti64 BM) and (<b>c</b>,<b>d</b>) HCF overview image with the arrow indicating failure initiation site and higher-magnification image of the crack propagation area (Ti6242 BM) that shows the fatigue striations in the inset image.</p>
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13 pages, 2981 KiB  
Article
Study on Cutting Chip in Milling GH4169 with Indexable Disc Cutter
by Gensheng Li, Chao Xian and Hongmin Xin
Materials 2021, 14(11), 3135; https://doi.org/10.3390/ma14113135 - 7 Jun 2021
Cited by 3 | Viewed by 2281
Abstract
The study and control for chip have a significant impact on machining quality and productivity. In this paper, GH4169 was cut with an indexable disc milling cutter. The chips corresponding to each group of cutting parameters were collected, and the chip parameters (chip [...] Read more.
The study and control for chip have a significant impact on machining quality and productivity. In this paper, GH4169 was cut with an indexable disc milling cutter. The chips corresponding to each group of cutting parameters were collected, and the chip parameters (chip curl radius, chip thickness deformation coefficient, and chip width deformation coefficient) were measured. The qualitative relationship between the chip parameters and cutting parameters was studied. The quadratic polynomial models between chip parameters and cutting parameters were established and verified. The results showed that the chip parameters (chip curl radius, chip thickness deformation coefficient and chip width deformation coefficient) were negatively correlated with spindle speed; chip parameters were positively correlated with feed speed; chip parameters were positively correlated with cutting depth. The maximum deviation rate between measured values and predicted values for chip curl radius was 9.37%; the maximum deviation rate for cutting thickness deformation coefficient was 13.8%, and the maximum deviation rate of cutting width deformation coefficient was 7.86%. It can be seen that the established models are accurate. The models have guiding significance for chip control. Full article
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<p>Disc milling cutter of indexable three-sided inserts.</p>
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<p>Position relationship of the three inserts.</p>
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<p>Insert.</p>
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<p>The positioning and clamping mode of inserts and cutter disc.</p>
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<p>Symmetrical milling.</p>
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<p>Chips.</p>
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<p>Geometric dimension of the chip breaking groove.</p>
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<p>Geometric dimension of the chip pocket for the disc cutter.</p>
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<p>Measurement of chip curl radius.</p>
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<p>Variation of chip curl radius with cutting parameters.</p>
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<p>Variation of chip thickness deformation coefficient with cutting parameters.</p>
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<p>Variation of chip width deformation coefficient with cutting parameters.</p>
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<p>Residual errors of chip curl radius.</p>
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<p>Residual errors of chip thickness deformation coefficient.</p>
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<p>Residual errors of chip width deformation coefficient.</p>
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<p>Comparison between the measured and predicted values for chip thickness deformation coefficient.</p>
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<p>Comparison between the measured and predicted values for chip curl radius.</p>
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<p>Comparison between the measured and predicted values for chip width deformation coefficient.</p>
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13 pages, 3421 KiB  
Article
Advanced Biofuels Based on Fischer–Tropsch Synthesis for Applications in Gasoline Engines
by Jiří Hájek, Vladimír Hönig, Michal Obergruber, Jan Jenčík, Aleš Vráblík, Radek Černý, Martin Pšenička and Tomáš Herink
Materials 2021, 14(11), 3134; https://doi.org/10.3390/ma14113134 - 7 Jun 2021
Cited by 6 | Viewed by 2945
Abstract
The aim of the article is to determine the properties of fuel mixtures of Fischer–Tropsch naphtha fraction with traditional gasoline (petrol) to be able to integrate the production of advanced alternative fuel based on Fischer–Tropsch synthesis into existing fuel markets. The density, octane [...] Read more.
The aim of the article is to determine the properties of fuel mixtures of Fischer–Tropsch naphtha fraction with traditional gasoline (petrol) to be able to integrate the production of advanced alternative fuel based on Fischer–Tropsch synthesis into existing fuel markets. The density, octane number, vapor pressure, cloud point, water content, sulphur content, refractive index, ASTM color, heat of combustion, and fuel composition were measured using the gas chromatography method PIONA. It was found that fuel properties of Fischer–Tropsch naphtha fraction is not much comparable to conventional gasoline (petrol) due to the high n-alkane content. This research work recommends the creation of a low-percentage mixture of 3 vol.% of FT naphtha fraction with traditional gasoline to minimize negative effects—similar to the current legislative limit of 5 vol.% of bioethanol in E5 gasoline. FT naphtha fraction as a biocomponent does not contain sulphur or polyaromatic hydrocarbons nor benzene. Waste materials can be processed by FT synthesis. Fischer–Tropsch synthesis can be considered a universal fuel—the naphtha fraction cut can be declared as a biocomponent for gasoline fuel without any further necessary catalytic upgrading. Full article
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<p>(<b>a</b>) Research octane number of FT–gasoline mixtures; (<b>b</b>) Motor octane number of FT–gasoline mixtures.</p>
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<p>Density of FT–gasoline mixtures.</p>
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<p>(<b>a</b>) Colour of FT–gasoline mixtures; (<b>b</b>) refractive index of FT–gasoline mixtures.</p>
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<p>(<b>a</b>) Distillation curve of FT–gasoline mixtures; (<b>b</b>) changes in temperature distillation of gasoline containing FT naphtha.</p>
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<p>Influence of FT–naphtha on E70, E100 and E150 of FT–gasoline mixtures.</p>
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<p>Vapour pressure of FT–gasoline mixtures.</p>
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<p>Vapour Lock Index (VLI) of FT–naphtha mixtures.</p>
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<p>PIONA composition of FT–gasoline mixtures.</p>
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15 pages, 3750 KiB  
Article
A Novel Dry Treatment for Municipal Solid Waste Incineration Bottom Ash for the Reduction of Salts and Potential Toxic Elements
by Marco Abis, Martina Bruno, Franz-Georg Simon, Raul Grönholm, Michel Hoppe, Kerstin Kuchta and Silvia Fiore
Materials 2021, 14(11), 3133; https://doi.org/10.3390/ma14113133 - 7 Jun 2021
Cited by 3 | Viewed by 2707
Abstract
The main obstacle to bottom ash (BA) being used as a recycling aggregate is the content of salts and potential toxic elements (PTEs), concentrated in a layer that coats BA particles. This work presents a dry treatment for the removal of salts and [...] Read more.
The main obstacle to bottom ash (BA) being used as a recycling aggregate is the content of salts and potential toxic elements (PTEs), concentrated in a layer that coats BA particles. This work presents a dry treatment for the removal of salts and PTEs from BA particles. Two pilot-scale abrasion units (with/without the removal of the fine particles) were fed with different BA samples. The performance of the abrasion tests was assessed through the analyses of particle size and moisture, and that of the column leaching tests at solid-to-liquid ratios between 0.3 and 4. The results were: the particle-size distribution of the treated materials was homogeneous (25 wt % had dimensions <6.3 mm) and their moisture halved, as well as the electrical conductivity of the leachates. A significant decrease was observed in the leachates of the treated BA for sulphates (44%), chlorides (26%), and PTEs (53% Cr, 60% Cu and 8% Mo). The statistical analysis revealed good correlations between chloride and sulphate concentrations in the leachates with Ba, Cu, Mo, and Sr, illustrating the consistent behavior of the major and minor components of the layer surrounding BA particles. In conclusion, the tested process could be considered as promising for the improvement of BA valorization. Full article
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<p>Grinding mechanisms: (<b>a</b>) compression, (<b>b</b>) chipping, (<b>c</b>) abrasion (adapted from Wills and Finch 2015 [<a href="#B27-materials-14-03133" class="html-bibr">27</a>]).</p>
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<p>Aggregate motion in a tumbling mill (adapted from Ali et al., 2019 [<a href="#B28-materials-14-03133" class="html-bibr">28</a>]; Wills 2016 [<a href="#B29-materials-14-03133" class="html-bibr">29</a>]; Wills and Finch 2015 [<a href="#B27-materials-14-03133" class="html-bibr">27</a>]).</p>
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<p>Particle size distribution of (<b>a</b>) the raw samples from Plant A and Plant B, of (<b>b</b>) samples treated for 60 min and of (<b>c</b>) samples treated for 120 min. Dotted line is mesh = 2 mm.</p>
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<p>Moisture content of the raw samples from Plant A and Plant B, of the samples treated for 60 and 120 min abrasion (Abr.) time, and those treated with the concrete mixer (only Plant B).</p>
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<p>Correlations between electrical conductivity and (<b>a</b>) chloride and (<b>b</b>) sulphate concentrations in the leachates.</p>
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<p>Trends of (<b>a</b>) chlorides and (<b>b</b>) sulphates’ cumulative release from the raw BA samples, and of (<b>c</b>) chlorides and (<b>d</b>) sulphates’ cumulative release after the abrasion tests (raw: untreated samples; CM: samples treated in the concrete mixer for 240 min; abr. 60 and abr. 120: samples treated in the sieving drum unit for 60 min and 120 min).</p>
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<p>Correlations between chlorides (<b>a1</b>–<b>a4</b>) and sulphates (<b>b1</b>–<b>b4</b>) and Ba, Cu, Mo, and Sr in the leachates derived from the column leaching tests.</p>
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17 pages, 3139 KiB  
Article
Improving the Properties of Degraded Soils from Industrial Areas by Using Livestock Waste with Calcium Peroxide as a Green Oxidizer
by Angelika Więckol-Ryk, Maciej Thomas and Barbara Białecka
Materials 2021, 14(11), 3132; https://doi.org/10.3390/ma14113132 - 7 Jun 2021
Cited by 3 | Viewed by 2525
Abstract
Over the past years, the treatment and use of livestock waste has posed a significant problem in environmental engineering. This paper outlines a new approach to application of calcium peroxide (CaO2) as a green oxidizer and microbiocidal agent in the treatment [...] Read more.
Over the past years, the treatment and use of livestock waste has posed a significant problem in environmental engineering. This paper outlines a new approach to application of calcium peroxide (CaO2) as a green oxidizer and microbiocidal agent in the treatment of poultry manure. It also presents the application of pretreated waste in improvement of degraded soils in industrial areas. The CCD (Central Composite Design) and RSM (Response Surface Methodology) were employed for optimizing the process parameters (CaO2 concentration 1.6–8.4 wt %, temperature 5.2–38.8 °C and contact time 7–209 h). The analysis of variance (ANOVA) was used to analyze the experimental results, which indicated good fit of the approximated to the experimental data (R2 = 0.8901, R2adj = 0.8168). The amendment of CaO2 in optimal conditions (8 wt % of CaO2, temperature 22 °C and contact time 108 h) caused a decrease in bacteria Escherichia coli (E. coli) in poultry manure from 8.7 log10 CFU/g to the acceptable level of 3 log10 CFU/g. The application of pretreated livestock waste on degraded soils and the studies on germination and growth of grass seed mixture (Lollum perenne—Naki, Lollum perenne—Grilla, Poa pratensis—Oxford, Festuca rubbra—Relevant, Festuca rubbra—Adio and Festuca trachypylla—Fornito) showed that a dose of 0.08 g of CaO2 per 1 gram of poultry manure induced higher yield of grass plants. The calculated indicators for growth of roots (GFR) and shoots (GFS) in soils treated with poultry manure were 10–20% lower compared to soils with amended CaO2. The evidence from this study suggests that CaO2 could be used as an environmentally friendly oxidizer and microbiocidal agent for livestock waste. Full article
(This article belongs to the Special Issue Processing of End-of-Life Materials and Industrial Wastes)
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<p>Soil sampling areas near the former “Miasteczko Śląskie” zinc smelter (<b>a</b>) and non-ferrous metals steelworks “Szopienice” (<b>b</b>).</p>
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<p>Bar-chart of the absolute value of standardized assessment of the effects (<span class="html-italic">E. coli</span>, log<sub>10</sub>CFU/g, 3 value, 1 block, 16 experiments, MS = 0.3877). L—linear effect and Q—quadratic effect.</p>
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<p>The correlation between the estimated and observed values (<span class="html-italic">E. coli</span>, log<sub>10</sub>CFU/g, 3 value, 1 block, 16 experiments, MS = 0.3877).</p>
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<p>The interactions between: (<b>A</b>) temperature (°C) and CaO<sub>2</sub> concentration (wt %), (<b>B</b>) contact time (h) and CaO<sub>2</sub> concentration (wt %) and (<b>C</b>) contact time (h) and temperature (°C).</p>
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<p>Pot samples with the grass seed mixture after 21 days of plant growth.</p>
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<p>Impact of poultry manure treated with calcium peroxide on roots and shoots length of the grass seed mixture.</p>
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19 pages, 12589 KiB  
Article
Numerical Investigation of Degradation of 316L Steel Caused by Cavitation
by Artur Maurin
Materials 2021, 14(11), 3131; https://doi.org/10.3390/ma14113131 - 7 Jun 2021
Cited by 5 | Viewed by 2285
Abstract
The degradation process of 316L stainless steel caused by cavitation was investigated by means of finite element analysis. The damage characteristics of metal specimens subjected to the cavitation bubble collapse process were recreated by simulation with a micro-jet water hammer. The simulation results [...] Read more.
The degradation process of 316L stainless steel caused by cavitation was investigated by means of finite element analysis. The damage characteristics of metal specimens subjected to the cavitation bubble collapse process were recreated by simulation with a micro-jet water hammer. The simulation results were compared with the cavitation pits created in the experimental tests. In the experiment, different inlet and outlet pressures in a test chamber with a system of barricade exciters differentiated the erosion process results. Hydrodynamic cavitation caused uneven distribution of the erosion over the specimens’ surface, which has been validated by roughness measurements, enabling localisation and identification of the shape and topography of the impact pits. The erosion rate of the steel specimens was high at the beginning of the test and decreased over time, indicating the phase transformation and/or the strain-hardening of the surface layer. A numerical simulation showed that the impact of the water micro-jet with a velocity of 100 m/s exceeds the tensile strength of 316L steel, and produces an impact pit. The subsequent micro-jet impact on the same zone deepens the pit depth only to a certain extent due to elastoplastic surface hardening. The correlation between post-impact pit geometry and impact velocity was investigated. Full article
(This article belongs to the Special Issue Erosion Resistance of Materials)
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<p>Schematic of the cavitation chamber test device [<a href="#B17-materials-14-03131" class="html-bibr">17</a>] (Reprinted from “Effect of cavitation intensity on degradation of X6CrNiTi18-10 stainless steel” by A.K. Krella, A. Krupa, Wear, Volumes 408–409, 2018, Pages 180-189, ISSN 0043-1648, Copyright under license no. 5057500490519 (2021), with permission from Elsevier).</p>
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<p>Johnson–Cook strength characteristics for 316L stainless steel.</p>
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<p>Cross section of numerical calculation domain with FE mesh.</p>
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<p>Degradation of 316L steel at low cavitation intensity (<math display="inline"><semantics> <mrow> <mi>p</mi> <mn>1</mn> <mo>=</mo> </mrow> </semantics></math> 600 kPa): (<b>a</b>) Damage in the slightly eroded area; (<b>b</b>) Damage in the severely eroded area [<a href="#B17-materials-14-03131" class="html-bibr">17</a>] (Reprinted from “Effect of cavitation intensity on degradation of X6CrNiTi18-10 stainless steel” by A.K. Krella, A. Krupa, Wear, Volumes 408–409, 2018, Pages 180-189, ISSN 0043-1648, Copyright under license no. 5057500490519 (2021), with permission from Elsevier).</p>
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<p>Profile of <math display="inline"><semantics> <mrow> <mi>R</mi> <mi>a</mi> </mrow> </semantics></math> roughness parameter of 316L steel exposed to cavitation at: (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>p</mi> <mn>1</mn> </mrow> </semantics></math> = 600 kPa; (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>p</mi> <mn>1</mn> </mrow> </semantics></math> = 700 kPa; (<b>c</b>) <math display="inline"><semantics> <mrow> <mi>p</mi> <mn>1</mn> </mrow> </semantics></math> = 800 kPa; (<b>d</b>) <math display="inline"><semantics> <mrow> <mi>p</mi> <mn>1</mn> </mrow> </semantics></math> = 900 kPa (marked points show the arithmetic mean calculated from the values of experimental data) [<a href="#B17-materials-14-03131" class="html-bibr">17</a>] (Reprinted from “Effect of cavitation intensity on degradation of X6CrNiTi18-10 stainless steel” by A.K. Krella, A. Krupa, Wear, Volumes 408–409, 2018, Pages 180-189, ISSN 0043-1648, Copyright under license no. 5057500490519 (2021), with permission from Elsevier).</p>
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<p>Von Mises stress distribution during first micro-jet impact at 100 m/s: (<b>a</b>) initial stage of the impact; (<b>b</b>) stage during the impact; (<b>c</b>) residual stress after the impact.</p>
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<p>Von Mises stress distribution during subsequent micro-jet impact at 100 m/s: (<b>a</b>) initial stage of the impact; (<b>b</b>) stage during the impact; (<b>c</b>) residual stress after the impact.</p>
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<p>Exceeded yield stress zone (over 307 MPa—red) of 316L stainless steel: (<b>a</b>) after first micro-jet impact; (<b>b</b>) after subsequent micro-jet impact; at 100 m/s.</p>
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<p>Von Mises stress distribution during first micro-jet impact at 200 m/s: (<b>a</b>) initial stage of the impact; (<b>b</b>) stage during the impact; (<b>c</b>) residual stress after the impact.</p>
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<p>Von Mises stress distribution during subsequent micro-jet impact at 200 m/s: (<b>a</b>) initial stage of the impact; (<b>b</b>) stage during the impact; (<b>c</b>) residual stress after the impact.</p>
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<p>Exceeded yield stress zone (over 307 MPa—red) of 316L stainless steel: (<b>a</b>) after first micro-jet impact; (<b>b</b>) after subsequent micro-jet impact; at 200 m/s.</p>
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<p>Von Mises stress distribution during first micro-jet impact at 500 m/s: (<b>a</b>) initial stage of the impact; (<b>b</b>) stage during the impact; (<b>c</b>) residual stress after the impact.</p>
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<p>Von Mises stress distribution during subsequent micro-jet impact at 200 m/s: (<b>a</b>) initial stage of the impact; (<b>b</b>) stage during the impact; (<b>c</b>) residual stress after the impact.</p>
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<p>Exceeded yield stress zone (over 307 MPa—red) of 316L stainless steel: (<b>a</b>) after first micro-jet impact; (<b>b</b>) after subsequent micro-jet impact; at 500 m/s.</p>
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19 pages, 3422 KiB  
Article
Linear Friction Welding of an AZ91 Magnesium Alloy and the Effect of Ca Additions on the Weld Characteristics
by Luis Angel Villegas-Armenta, Priti Wanjara, Javad Gholipour, Isao Nakatsugawa, Yasumasa Chino and Mihriban Pekguleryuz
Materials 2021, 14(11), 3130; https://doi.org/10.3390/ma14113130 - 7 Jun 2021
Cited by 4 | Viewed by 2905
Abstract
Solid-state welding offers distinct advantages for joining reactive materials, such as magnesium (Mg) and its alloys. This study investigates the effect of linear friction welding (LFW) on the microstructure and mechanical properties of cast AZ91 (Mg–9Al–1Zn) and AZ91–2Ca alloys, which (to the best [...] Read more.
Solid-state welding offers distinct advantages for joining reactive materials, such as magnesium (Mg) and its alloys. This study investigates the effect of linear friction welding (LFW) on the microstructure and mechanical properties of cast AZ91 (Mg–9Al–1Zn) and AZ91–2Ca alloys, which (to the best knowledge of the authors) has not been reported in the literature. Using the same set of LFW process parameters, similar alloy joints—namely, AZ91/AZ91 and AZ91–2Ca/AZ91–2Ca—were manufactured and found to exhibit integral bonding at the interface without defects, such as porosity, inclusions, and/or cracking. Microstructural examination of the AZ91/AZ91 joint revealed dissolution of the Al-rich second phase in the weld zone, while the Mn containing phases remained and were refined. In the AZ91–2Ca/AZ91–2Ca joint, the weld zone retained Ca- and Mn-rich phases, which were also refined due to the LFW process. In both joint types, extensive recrystallization occurred during LFW, as evidenced by the refinement of the grains from ~1000 µm in the base materials to roughly 2–6 µm in the weld zone. These microstructural changes in the AZ91/AZ91 and AZ91–2Ca/AZ91–2Ca joints increased the hardness in the weld zone by 32%. The use of digital image correlation for strain mapping along the sample gage length during tensile testing revealed that the local strains were about 50% lower in the weld zone relative to the AZ91 and AZ91–2Ca base materials. This points to the higher strength of the weld zone in the AZ91/AZ91 and AZ91–2Ca/AZ91–2Ca joints due to the fine grain size, second phase refinement, and strong basal texture. Final fracture during tensile loading of both joints occurred in the base materials. Full article
(This article belongs to the Special Issue Welding and Joining of Materials for Advanced Aerospace Applications)
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<p>Schematic diagram showing (<b>a</b>) the LFW coupon length (L), width (W), and depth (D); (<b>b</b>) the machining plan for extracting the metallography and tensile samples; and (<b>c</b>) the geometry of the tensile samples.</p>
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<p>Front and side images of the welded (<b>a</b>,<b>b</b>) AZ91 and (<b>c</b>,<b>d</b>) AZ91–2Ca. Both similar Mg alloy welds display discontinuous flash formation.</p>
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<p>Thermal camera temperature readings at the joint interface and the evolution in the average temperature at the joint interface surface for AZ91 (<b>a</b>,<b>c</b>) and AZ91–2Ca (<b>b</b>,<b>d</b>) during LFW.</p>
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<p>Stereoscopic images of the weld cross-sections (<b>a</b>) AZ91/AZ91 and (<b>b</b>) AZ91–2Ca/AZ91–2Ca alloys. The dotted lines represent the boundaries of the weld zone.</p>
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<p>XRD spectra for both the central weld zone and base material in (<b>a</b>) AZ91/AZ91 and (<b>b</b>) AZ91–2Ca/AZ91–2Ca welds.</p>
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<p>SEM micrographs of the (<b>a</b>) AZ91 and (<b>b</b>) AZ91–2Ca alloys. Both alloys contain the β–Mg<sub>17</sub>(Al, Zn)<sub>12</sub> (bulk and lamellar) and Al<sub>8</sub>Mn<sub>5</sub> phases. The addition of Ca to AZ91 forms the Al<sub>2</sub>Ca phase.</p>
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<p>AZ91/AZ91 weld. SEM micrographs of (<b>a</b>) the transition between the base material (bottom) and the central weld zone (top), (<b>b</b>) the central weld zone, and (<b>c</b>) a β–Mg<sub>17</sub>(Al, Zn)<sub>12</sub> particle located close to the central weld zone. Start of central weld zone in the AZ91/AZ91 weld (<b>d</b>) is shown along with its EDS elemental maps (<b>e</b>–<b>h</b>). Al and Zn concentrated initially at the β–Mg<sub>17</sub>(Al, Zn)<sub>12</sub> phase, while Mn remained in the Al<sub>8</sub>Mn<sub>5</sub> phase. After welding, they dissolved into the Mg matrix.</p>
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<p>AZ91–2Ca/AZ91–2Ca weld. SEM micrographs of (<b>a</b>) the weld region between the base material (bottom) and the central weld zone (top), (<b>b</b>) the central weld zone, and (<b>c</b>) fragmentation of Al<sub>2</sub>Ca particles close to the central weld zone.</p>
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<p>(<b>a</b>) AZ91–2Ca/AZ91–2Ca weld. (<b>b</b>–<b>e</b>) EDS elemental mapping of the weld region between the base material (bottom) and the central weld zone (top). Al (<b>c</b>) is seen in the Al<sub>2</sub>Ca particles, while Zn (<b>d</b>) appears to be dispersed in the matrix. Mn (<b>e</b>) remained in the Al<sub>8</sub>Mn<sub>5</sub> phase. Towards the weld region, Ca (<b>f</b>) predominates in the smaller particles.</p>
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<p>Cast alloys of (<b>a</b>) AZ91 and (<b>b</b>) AZ91–2Ca before the LFW process. Large grains and thick dendrite arms are observed.</p>
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<p>EBSD maps and associated pole figures of the central weld zones in (<b>a</b>,<b>b</b>) AZ91/AZ91 and (<b>c</b>,<b>d</b>) AZ91–2Ca/AZ91–2Ca welds, where PD is forging direction, LD is longitudinal direction, and TD is transversal direction. Both weld zones display extensive recrystallization and a strong basal texture perpendicular to the forging direction and (<b>e</b>) tensile loading direction.</p>
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<p>Vickers microhardness maps for the weld region of (<b>a</b>) AZ91/AZ91 and (<b>b</b>) AZ91–2Ca/AZ91–2Ca welds. As the measurements approached the central weld zone, the hardness increased.</p>
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<p>Surface strain map for the (<b>a</b>) AZ91/AZ91 and (<b>b</b>) AZ91–2Ca/AZ91–2Ca welds right before the final fracture during tensile testing. The black dotted line shows the joint interface. In both welds, fracture occurred in the area of strain localization, outside the weld region (i.e., in the base material regions).</p>
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11 pages, 3036 KiB  
Article
Tuning of the Structure and Magnetocaloric Effect of Mn1−xZrxCoGe Alloys (Where x = 0.03, 0.05, 0.07, and 0.1)
by Karolina Kutynia and Piotr Gębara
Materials 2021, 14(11), 3129; https://doi.org/10.3390/ma14113129 - 7 Jun 2021
Cited by 5 | Viewed by 2303
Abstract
The aim of the present work is to study the influence of a partial substitution of Mn by Zr in MnCoGe alloys. The X-ray diffraction (XRD) studies revealed a coexistence of the orthorhombic TiNiSi-type and hexagonal Ni2In- type phases. The Rietveld [...] Read more.
The aim of the present work is to study the influence of a partial substitution of Mn by Zr in MnCoGe alloys. The X-ray diffraction (XRD) studies revealed a coexistence of the orthorhombic TiNiSi-type and hexagonal Ni2In- type phases. The Rietveld analysis showed that the changes in lattice constants and content of recognized phases depended on the Zr addition. The occurrence of structural transformation was detected. This transformation was confirmed by analysis of the temperature dependence of exponent n given in the relation ΔSM = C·(BMAX)n. A decrease of the Curie temperature with an increase of the Zr content in the alloy composition was detected. The magnetic entropy changes were 6.93, 13.42, 3.96, and 2.94 J/(kg K) for Mn0.97Zr0.03CoGe, Mn0.95Zr0.05CoGe, Mn0.93Zr0.07CoGe, and Mn0.9Zr0.1CoGe, respectively. A significant rise in the magnetic entropy change for samples doped by Zr (x = 0.05) was caused by structural transformation. Full article
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<p>Full Heusler alloy structure model [<a href="#B19-materials-14-03129" class="html-bibr">19</a>].</p>
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<p>Half-Heusler alloy structure model [<a href="#B20-materials-14-03129" class="html-bibr">20</a>].</p>
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<p>The XRD patterns collected for all studied samples.</p>
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<p>The Zr content dependence of the lattice constant of the analyzed unit cells. Errors were not matched as they were smaller than the symbol size. (<b>a</b>) Zr content of lattice parameters (a<sub>ort</sub> and c<sub>hex</sub>); (<b>b</b>) Zr content of lattice parameters (a<sub>hex</sub>, b<sub>ort</sub> and c<sub>ort</sub>/(3)<sup>1/2</sup>).</p>
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<p>The temperature dependences of magnetization collected under the external magnetic field of 0.01 T for all studied samples. Values were normalized to their maximum value.</p>
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<p>The temperature dependences of the magnetic entropy changes calculated for Mn<sub>0.97</sub>Zr<sub>0.03</sub>CoGe (<b>a</b>), Mn<sub>0.95</sub>Zr<sub>0.05</sub>CoGe (<b>b</b>), Mn<sub>0.93</sub>Zr<sub>0.07</sub>CoGe (<b>c</b>), and Mn<sub>0.9</sub>Zr<sub>0.1</sub>CoGe (<b>d</b>) alloys.</p>
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<p>The temperature dependences of the magnetic entropy changes calculated for Mn<sub>0.97</sub>Zr<sub>0.03</sub>CoGe (<b>a</b>), Mn<sub>0.95</sub>Zr<sub>0.05</sub>CoGe (<b>b</b>), Mn<sub>0.93</sub>Zr<sub>0.07</sub>CoGe (<b>c</b>), and Mn<sub>0.9</sub>Zr<sub>0.1</sub>CoGe (<b>d</b>) alloys under the change of external magnetic field ~5 T.</p>
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<p>The temperature dependences of the exponent n calculated for all investigated samples.</p>
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17 pages, 3954 KiB  
Article
Novel Triarylamine-Based Hole Transport Materials: Synthesis, Characterization and Computational Investigation
by Laila M. Nhari, Reda M. El-Shishtawy, Qiuchen Lu, Yuanzuo Li and Abdullah M. Asiri
Materials 2021, 14(11), 3128; https://doi.org/10.3390/ma14113128 - 7 Jun 2021
Cited by 3 | Viewed by 21357
Abstract
Three novel triarylamine-based electron-rich chromophores were synthesized and fully characterized. Compounds 1 and 2 were designed with electron-rich triphenylamine skeleton bearing two and four decyloxy groups namely, 3,4-bis(decyloxy)-N,N-diphenylaniline and N-(3,4-bis(decyloxy)phenyl)-3,4-bis(decyloxy)-N-phenylaniline, respectively. The well-known electron-rich phenothiazine was introduced to [...] Read more.
Three novel triarylamine-based electron-rich chromophores were synthesized and fully characterized. Compounds 1 and 2 were designed with electron-rich triphenylamine skeleton bearing two and four decyloxy groups namely, 3,4-bis(decyloxy)-N,N-diphenylaniline and N-(3,4-bis(decyloxy)phenyl)-3,4-bis(decyloxy)-N-phenylaniline, respectively. The well-known electron-rich phenothiazine was introduced to diphenylamine moiety through a thiazole ring to form N,N-bis(3,4-bis(decyloxy)phenyl)-5-(10H-phenothiazin-2-yl)thiazol-2-amine (Compound 3). These three novel compounds were fully characterized and their UV–vis absorption indicated their transparency as a favorable property for hole transport materials (HTMs) suitable for perovskite solar cells. Cyclic voltammetry measurements revealed that the HOMO energy levels were in the range 5.00–5.16 eV for all compounds, indicating their suitability with the HOMO energy level of the perovskite photosensitizer. Density functional theory (DFT) and time-dependent DFT (TD-DFT) have been used to investigate the possibility of the synthesized compounds to be utilized as HTMs for perovskite solar cells (PSCs). The computational investigation revealed that the hole mobility of Compound 1 was 1.08 × 10−2 cm2 V−1 s−1, and the substitution with two additional dialkoxy groups on the second phenyl ring as represented by Compound 2 significantly boosted the hole mobility to reach the value 4.21 × 10−2 cm2 V−1 s−1. On the other hand, Compound 3, in which the third phenyl group was replaced by a thiazole-based phenothiazine, the value of hole mobility decreased to reach 5.93 × 10−5 cm2 V−1 s−1. The overall results indicate that these three novel compounds could be promising HTMs for perovskite solar cells. Full article
(This article belongs to the Special Issue New Hole Transporting Materials for Perovskite Solar Cells)
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<p>The experimental UV–Vis absorption spectra of the compounds in DCM solutions (10<sup>−5</sup> mol/L).</p>
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<p>Cyclic voltammogram of <b>Compound 1</b> in DCM solution (10<sup>−3</sup> M).</p>
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<p>Cyclic voltammogram of <b>Compound 2</b> in DCM solution (10<sup>−3</sup> M).</p>
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<p>Cyclic voltammogram of <b>Compound 3</b> in DCM solution (10<sup>−3</sup> M).</p>
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<p>The molecular orbitals HOMO and LUMO of the three original molecules.</p>
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<p>Energy level diagram of the investigated hole transporting materials.</p>
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<p>Partial density of states graphs of three compounds.</p>
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<p>The computed UV–Vis absorption spectra of the compounds.</p>
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<p>Synthesis of Compounds <b>1–3</b>.</p>
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14 pages, 6104 KiB  
Article
Atomic Simulations of Packing Structures, Local Stress and Mechanical Properties for One Silicon Lattice with Single Vacancy on Heating
by Feng Dai, Dandan Zhao and Lin Zhang
Materials 2021, 14(11), 3127; https://doi.org/10.3390/ma14113127 - 7 Jun 2021
Cited by 4 | Viewed by 2009
Abstract
The effect of vacancy defects on the structure and mechanical properties of semiconductor silicon materials is of great significance to the development of novel microelectronic materials and the processes of semiconductor sensors. In this paper, molecular dynamics is used to simulate the atomic [...] Read more.
The effect of vacancy defects on the structure and mechanical properties of semiconductor silicon materials is of great significance to the development of novel microelectronic materials and the processes of semiconductor sensors. In this paper, molecular dynamics is used to simulate the atomic packing structure, local stress evolution and mechanical properties of a perfect lattice and silicon crystal with a single vacancy defect on heating. In addition, their influences on the change in Young’s modulus are also analyzed. The atomic simulations show that in the lower temperature range, the existence of vacancy defects reduces the Young’s modulus of the silicon lattice. With the increase in temperature, the local stress distribution of the atoms in the lattice changes due to the migration of the vacancy. At high temperatures, the Young’s modulus of the silicon lattice changes in anisotropic patterns. For the lattice with the vacancy, when the temperature is higher than 1500 K, the number and degree of distortion in the lattice increase significantly, the obvious single vacancy and its adjacent atoms contracting inward structure disappears and the defects in the lattice present complex patterns. By applying uniaxial tensile force, it can be found that the temperature has a significant effect on the elasticity–plasticity behaviors of the Si lattice with the vacancy. Full article
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<p>(<b>a</b>) Perfect Si lattice; (<b>b</b>) Si lattice with one vacancy.</p>
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<p>The average potential energy per atom varying with the temperature.</p>
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<p>Variation of Young’s modulus with the temperature: (<b>a</b>) perfect lattice with a temperature increase of 100 K; (<b>b</b>) lattice with one vacancy with a temperature increase of 100 K; (<b>c</b>) perfect lattice with a temperature increase of 20 K; (<b>d</b>) lattice with one vacancy with a temperature increase of 20 K.</p>
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<p>The atomic packing structure and the pressure distribution of Si lattice with one vacancy at different temperatures: (<b>a<sub>1</sub></b>–<b>a<sub>3</sub></b>) 300, (<b>b<sub>1</sub></b>–<b>b<sub>3</sub></b>) 400, (<b>c<sub>1</sub></b>–<b>c<sub>3</sub></b>) 700, (<b>d<sub>1</sub></b>–<b>d<sub>3</sub></b>) 1200 and (<b>e<sub>1</sub></b>–<b>e<sub>3</sub></b>) 1500 K; the black dotted line shows the packing structure and the pressure of the nearest neighbor atoms of vacancy, while the orange dotted line shows the packing structure and the pressure of the atoms neighboring the vacancy; the red atoms in this figure indicate that the atom undergoes compression, and the pressure is positive. The atomic pressure of dark red atoms is higher than that of light red atoms. Blue atoms are stretched, and the pressure is negative. Dark blue color indicates atoms that are under less pressure than light blue atoms.</p>
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<p>Stress varying with the strain and pressure distribution of (<b>a</b>) the prefect Si lattice and the Si lattice with one vacancy at 300 K, (<b>b</b>) the Si lattice with one vacancy at 1200 and (<b>c</b>) 1300 K along the [100] axis. The pictures on the right shows the packing structures corresponding to the letters at different strains on the left.</p>
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<p>Variations of yield strength and tensile strength of the Si lattice with temperature; (<b>a</b>) a temperature increase of 100 K; and (<b>b</b>) a temperature increase of 20 K.</p>
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11 pages, 1595 KiB  
Article
Comparative Evaluation of Mineral Trioxide Aggregate Obturation Using Four Different Techniques—A Laboratory Study
by Abhishek Isaac Mathew, Silvia Chamin Lee, Giampiero Rossi-Fedele, George Bogen, Venkateshbabu Nagendrababu and William Nguyen Ha
Materials 2021, 14(11), 3126; https://doi.org/10.3390/ma14113126 - 7 Jun 2021
Cited by 1 | Viewed by 4096
Abstract
This study aimed to compare the density of mineral trioxide aggregate (MTA) as a root canal filling material in the apical 5 mm of artificial root canals. Forty transparent acrylic blocks with 30-degree curved canals were instrumented and allocated into four compaction technique [...] Read more.
This study aimed to compare the density of mineral trioxide aggregate (MTA) as a root canal filling material in the apical 5 mm of artificial root canals. Forty transparent acrylic blocks with 30-degree curved canals were instrumented and allocated into four compaction technique groups (n = 10): Lawaty (hand files); gutta-percha (GP) points; auger (nickel–titanium rotary files in reverse mode); and plugger technique. Filled canals were weighed after setting the MTA to calculate difference in mass. Two postoperative radiographs compared radiopacity by measuring luminance variations at 0.5 mm, 1 mm, 2 mm, 3 mm, 4 mm, and 5 mm from the root apex. Obturation time was measured using a digital chronometer. The significance level was set to p < 0.05. The plugger group had a lower mass. Relative luminance was significantly higher for the Lawaty group than the plugger group at all examined apical levels. The relative luminance of the auger and GP groups were significantly higher than the plugger group at depths between 0.5 mm and 2 mm. Relative luminance was highest for the Lawaty technique at all depths between 0.5 mm and 4 mm. The Lawaty technique group was associated with increased obturation time compared with pluggers. Compacting MTA in curved canals with the Lawaty technique has the highest mass and radiopacity but requires more time. Full article
(This article belongs to the Special Issue Dental Materials in Endodontic and Post-endodontic Therapy)
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<p>Experimental design: (<b>a</b>) acrylic block used with a custom-made composite resin crown; (<b>b</b>) acrylic block model after placement in the maxillary tooth mould of the phantom head; (<b>c</b>) MTA delivered to the canal using a hand file; (<b>d</b>) MTA placed into the canal using a rotary file (ProTaper Gold<sup>®</sup> F2 not used in image); (<b>e</b>) MTA canal delivery using a GP point; and (<b>f</b>) MTA transferred to the canal using a plugger.</p>
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<p>The Lawaty technique: hand files used to carry and pack MTA sequentially in a “step-back” method.</p>
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<p>Comparison of the estimated mean values for relative luminance for each group at various depths from the apical end. Estimated differences in mean relative luminance compared to the plugger group generally decreased as the distance from the apex increased.</p>
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<p>Representative radiographs from each group showing the apical 5 mm: (<b>a</b>) Lawaty group; (<b>b</b>) auger group; (<b>c</b>) GP group; and (<b>d</b>) the plugger group. Orange arrows indicate areas of reduced relative luminescence. The red arrow shows that the obturation is short of working length (also an area of reduced relative luminance).</p>
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12 pages, 4465 KiB  
Article
Elastic Properties and Energy Loss Related to the Disorder–Order Ferroelectric Transitions in Multiferroic Metal–Organic Frameworks [NH4][Mg(HCOO)3] and [(CH3)2NH2][Mg(HCOO)3]
by Zhiying Zhang, Hongliang Yu, Xin Shen, Lei Sun, Shumin Yue and Hao Tang
Materials 2021, 14(11), 3125; https://doi.org/10.3390/ma14113125 - 7 Jun 2021
Cited by 2 | Viewed by 2284
Abstract
Elastic properties are important mechanical properties which are dependent on the structure, and the coupling of ferroelasticity with ferroelectricity and ferromagnetism is vital for the development of multiferroic metal–organic frameworks (MOFs). The elastic properties and energy loss related to the disorder–order ferroelectric transition [...] Read more.
Elastic properties are important mechanical properties which are dependent on the structure, and the coupling of ferroelasticity with ferroelectricity and ferromagnetism is vital for the development of multiferroic metal–organic frameworks (MOFs). The elastic properties and energy loss related to the disorder–order ferroelectric transition in [NH4][Mg(HCOO)3] and [(CH3)2NH2][Mg(HCOO)3] were investigated using differential scanning calorimetry (DSC) and dynamic mechanical analysis (DMA). The DSC curves of [NH4][Mg(HCOO)3] and [(CH3)2NH2][Mg(HCOO)3] exhibited anomalies near 256 K and 264 K, respectively. The DMA results illustrated the minimum in the storage modulus and normalized storage modulus, and the maximum in the loss modulus, normalized loss modulus and loss factor near the ferroelectric transition temperatures of 256 K and 264 K, respectively. Much narrower peaks of loss modulus, normalized loss modulus and loss factor were observed in [(CH3)2NH2][Mg(HCOO)3] with the peak temperature independent of frequency, and the peak height was smaller at a higher frequency, indicating the features of first-order transition. Elastic anomalies and energy loss in [NH4][Mg(HCOO)3] near 256 K are due to the second-order paraelectric to ferroelectric phase transition triggered by the disorder–order transition of the ammonium cations and their displacement within the framework channels, accompanied by the structural phase transition from the non-polar hexagonal P6322 to polar hexagonal P63. Elastic anomalies and energy loss in [(CH3)2NH2][Mg(HCOO)3] near 264 K are due to the first-order paraelectric to ferroelectric phase transitions triggered by the disorder–order transitions of alkylammonium cations located in the framework cavities, accompanied by the structural phase transition from rhombohedral R3¯c to monoclinic Cc. The elastic anomalies in [NH4][Mg(HCOO)3] and [(CH3)2NH2][Mg(HCOO)3] showed strong coupling of ferroelasticity with ferroelectricity. Full article
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<p>OM image of (<b>a</b>) [NH<sub>4</sub>][Mg(HCOO)<sub>3</sub>] and (<b>b</b>) [(CH<sub>3</sub>)<sub>2</sub>NH<sub>2</sub>][Mg(HCOO)<sub>3</sub>] crystals.</p>
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<p>SEM image of (<b>a</b>) [NH<sub>4</sub>][Mg(HCOO)<sub>3</sub>] and (<b>b</b>) [(CH<sub>3</sub>)<sub>2</sub>NH<sub>2</sub>][Mg(HCOO)<sub>3</sub>] crystals.</p>
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<p>Rietveld fit of XRD patterns of (<b>a</b>) [NH<sub>4</sub>][Mg(HCOO)<sub>3</sub>] and (<b>b</b>) [(CH<sub>3</sub>)<sub>2</sub>NH<sub>2</sub>][Mg(HCOO)<sub>3</sub>] at room temperature.</p>
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<p>Structures of (<b>a</b>) [NH<sub>4</sub>][Mg(HCOO)<sub>3</sub>] and (<b>b</b>) [(CH<sub>3</sub>)<sub>2</sub>NH<sub>2</sub>][Mg(HCOO)<sub>3</sub>] at room temperature.</p>
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<p>DSC curves of (<b>a</b>) [NH<sub>4</sub>][Mg(HCOO)<sub>3</sub>] and (<b>b</b>) [(CH<sub>3</sub>)<sub>2</sub>NH<sub>2</sub>][Mg(HCOO)<sub>3</sub>] during cooling and heating processes at the rate of 5 K/min.</p>
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<p>Temperature dependences of (<b>a</b>) storage modulus E’, (<b>b</b>) loss modulus E’’, (<b>c</b>) loss factor tanδ of [NH<sub>4</sub>][Mg(HCOO)<sub>3</sub>] single crystals, (<b>d</b>) normalized storage modulus E’<sub>T</sub>/E’<sub>280</sub>, (<b>e</b>) normalized loss modulus E’’<sub>T</sub>/E’’<sub>298</sub> and (<b>f</b>) loss factor tanδ of [NH<sub>4</sub>][Mg(HCOO)<sub>3</sub>] pellet determined by DMA during heating at the rate of 2 K/min. The vertical dash-dotted line indicates the ferroelectric transition temperature of 256 K.</p>
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<p>Temperature dependences of (<b>a</b>) storage modulus E’, (<b>b</b>) loss modulus E’’, (<b>c</b>) loss factor tanδ of [NH<sub>4</sub>][Mg(HCOO)<sub>3</sub>] single crystals, (<b>d</b>) normalized storage modulus E’<sub>T</sub>/E’<sub>280</sub>, (<b>e</b>) normalized loss modulus E’’<sub>T</sub>/E’’<sub>298</sub> and (<b>f</b>) loss factor tanδ of [NH<sub>4</sub>][Mg(HCOO)<sub>3</sub>] pellet determined by DMA during heating at the rate of 2 K/min. The vertical dash-dotted line indicates the ferroelectric transition temperature of 256 K.</p>
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<p>Temperature dependences of (<b>a</b>) storage modulus E’, (<b>b</b>) loss modulus E’’, (<b>c</b>) loss factor tanδ of [(CH<sub>3</sub>)<sub>2</sub>NH<sub>2</sub>][Mg(HCOO)<sub>3</sub>] single crystals, (<b>d</b>) normalized storage modulus E’<sub>T</sub>/E’<sub>298</sub>, (<b>e</b>) normalized loss modulus E’’<sub>T</sub>/E’’<sub>298</sub> and (<b>f</b>) loss factor tanδ of [(CH<sub>3</sub>)<sub>2</sub>NH<sub>2</sub>][Mg(HCOO)<sub>3</sub>] pellet determined by DMA during heating at the rate of 2 K/min. The vertical dash-dotted line indicates the ferroelectric transition temperature of 264 K.</p>
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<p>Double logarithmic plot ln(tanδ) vs. ln(f) for the peak in the temperature dependence of tanδ near 260 K in [NH<sub>4</sub>][Mg(HCOO)<sub>3</sub>] (<b>a</b>) and near 270 K in [(CH<sub>3</sub>)<sub>2</sub>NH<sub>2</sub>][Mg(HCOO)<sub>3</sub>] (<b>b</b>).</p>
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22 pages, 9140 KiB  
Article
Analysis of Microstructure and Mechanical Properties of AlSi11 after Chip Recycling, Co-Extrusion, and Arc Welding
by Piotr Noga, Lechosław Tuz, Krzysztof Żaba and Adam Zwoliński
Materials 2021, 14(11), 3124; https://doi.org/10.3390/ma14113124 - 7 Jun 2021
Cited by 14 | Viewed by 2747
Abstract
Recycling of raw materials and is crucial for the production of new products for the global economy. The aim here is, on the one hand, to reduce energy consumption, and, on the other hand, to obtain materials with similar functional properties. The study [...] Read more.
Recycling of raw materials and is crucial for the production of new products for the global economy. The aim here is, on the one hand, to reduce energy consumption, and, on the other hand, to obtain materials with similar functional properties. The study undertook research on the possibility of processing AlSi11 aluminum chips by compaction and co-extruding to obtain a product in the form of a flat bar with mechanical properties not lower than those of the cast materials. The performed tests and the developed technique allowed to obtain flat bars with more favorable mechanical properties (Yield Strength YS ≥ 155 MPa; Ultimate Tensile Strength UTS ≥ 212 MPa) than the castings (YS ≥ 70 MPa ≥ 150 MPa). The weldability evaluation tests revealed that the material is susceptible to porosity. The presence of pores, which reduces the cross-section (up to 60%), reduces the tensile strength (up to 20 MPa). The typical joint structure and plasticity is obtained, which indicate the possibility of tensile strength improvement. Full article
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<p>Manufacturing process of materials for tests.</p>
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<p>Chips after machining: (<b>A</b>) milling, (<b>B</b>) turning.</p>
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<p>Laboratory installation for extrusion: (<b>A</b>) cold compaction, (<b>B</b>) hot co-extrusion.</p>
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<p>Recycled material for tests after: (<b>A</b>) casting, (<b>B</b>) fine chips consolidation, (<b>C</b>) large chips consolidation.</p>
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<p>Plates beveling for welding.</p>
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<p>Test range for profiles after extrusion (green dot line) and welded joints (red dot line).</p>
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<p>Flat bars after hot co-extrusion from: (<b>A</b>)—cast (M1), (<b>B</b>)—large chips (M2); (<b>C</b>)—fine chips (M3); surface morphology with lack of cracks.</p>
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<p>Microstructure in cross-section of extruded bars: (<b>A</b>) M1; (<b>B</b>) M2; (<b>C</b>) M3; visible main phases in microstructure (LM) and surface morphology in cross-section (SEM) with porosity of cast metal (<b>A</b>) and discontinuities of fine chips bar (<b>C</b>).</p>
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<p>Elements distribution in cross-section of bars made by: (<b>A</b>) cast (M1), (<b>B</b>) large chips (M2), (<b>C</b>) fine chips (M3); visible refinement of structure without chemical composition changes.</p>
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<p>Stress–strain (elongation) curves for extruded bars.</p>
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<p>Fractures after tensile test (LM/SEM) of: (<b>A</b>) M1; (<b>B</b>) M2, (<b>C</b>) M3; ductile fracture in all samples.</p>
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<p>Face of welded joints:, (<b>A</b>) W1—correct shape, (<b>B</b>) W2—fine pores, (<b>C</b>) W3—strong porosity.</p>
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<p>Macrostructure of welded joints: (<b>A</b>) W1, (<b>B</b>) W2, (<b>C</b>) W3; yellow arrows indicate the porosity; red arrow indicate small porosity visible on the face of the weld.</p>
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<p>Microstructure of joint W1: (<b>A</b>) general view, microstructure of: (<b>B</b>) BM with coarse particles, (<b>C</b>) HAZ with refined particles near to fusion line, (<b>D</b>) weld with dendritic structure and eutectics in the inter-dendritic areas, (<b>E</b>) analysis of distribution of the most important elements in the weld metal (red rectangular indicate the EDS placement).</p>
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<p>Microstructure of joint W2: (<b>A</b>) general view, microstructure of: (<b>B</b>) BM with coarse particles; (<b>C</b>) HAZ with refined particles near to fusion line; (<b>D</b>) weld with dendritic structure and eutectics in the inter-dendritic areas; visible porosity in HAZ and weld; (<b>E</b>) analysis of distribution of the most important elements in the weld metal (red rectangular indicate the EDS placement).</p>
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<p>Microstructure of joint W3: (<b>A</b>) general view; microstructure of: (<b>B</b>) BM with coarse particles; (<b>C</b>) HAZ with refined particles near to fusion line; (<b>D</b>) weld with dendritic structure and eutectics in the inter-dendritic areas; visible porosity in HAZ and weld; (<b>E</b>) analysis of distribution of the most important elements in the weld metal (red rectangular indicate the EDS placement).</p>
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<p>Stress–strain curves for the welded joins W1, W2, W3.</p>
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<p>Quasi-ductile fracture of welded joints; visible porosity of W2 and W3; (<b>A</b>) W1—visible large Si precipitation, (<b>B</b>) W2, (<b>C</b>) W3.</p>
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<p>Surface of pore with visible effect of crystallization.</p>
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<p>Hardness distribution in the cross-section of the welded joint: (<b>A</b>) W1, (<b>B</b>) W2, (<b>C</b>) W3.</p>
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14 pages, 5386 KiB  
Article
Damage Development on the Surface of Nickel Coating in the Initial Period of Erosion
by Dominika E. Zakrzewska, Marta H. Buszko, Alicja K. Krella, Anna Komenda, Grzegorz Mordarski and Robert P. Socha
Materials 2021, 14(11), 3123; https://doi.org/10.3390/ma14113123 - 7 Jun 2021
Cited by 7 | Viewed by 2601
Abstract
The common occurrence of the phenomenon of cavitation in many industries and the multitude of factors affecting the resistance to cavitation erosion of used materials contribute to the search for methods and appropriate parameters of coating application that are able to minimize the [...] Read more.
The common occurrence of the phenomenon of cavitation in many industries and the multitude of factors affecting the resistance to cavitation erosion of used materials contribute to the search for methods and appropriate parameters of coating application that are able to minimize the effects of erosion. To determine the validity of the developed application parameters and the method used, cavitation studies and microscopic observations of the development of erosion during the cavitation test were carried out. There was a clear lack of incubation time and a linear increase in losses after 60 min of the test. Moreover, the damage observed during the test overlapped, widening the area of erosion and thus leading to damage to the integrity of the coating. Full article
(This article belongs to the Special Issue Erosion Resistance of Materials)
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<p>Scheme of the system for measuring the resting potential.</p>
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<p>Nickel coating before cavitation erosion tests: (<b>a</b>) surface morphology with roughness profiles along the selected measurement lines; (<b>b</b>) 3D profile of a surface defect.</p>
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<p>Force versus indentation depth curves for a Ni–P coating: (<b>a</b>) hardness and elastic modulus change with loading cycle (<b>b</b>).</p>
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<p>The dependence of the electrode potential versus the time after immersion to 3.5% NaCl solution.</p>
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<p>Results of the cavitation erosion of nickel coating: (<b>a</b>) volume loss in time and (<b>b</b>) cumulative erosion rates in time.</p>
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<p>Nickel coating after 5 min of the cavitation erosion tests: (<b>a</b>) surface morphology with roughness profile along the selected measurement line; (<b>b</b>) 3D surface profile of a pit.</p>
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<p>Nickel coating after 10 min of the cavitation erosion tests: (<b>a</b>) surface morphology with roughness profile along the selected measurement line; (<b>b</b>) 3D surface profile.</p>
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<p>Nickel coating after 30 min of the cavitation erosion tests: (<b>a</b>) surface morphology with roughness profile along the selected measurement line; (<b>b</b>) 3D surface profile.</p>
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<p>Nickel coating after 60 min of the cavitation erosion tests: (<b>a</b>) surface morphology with roughness profile along the selected measurement line; (<b>b</b>) 3D surface profile.</p>
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11 pages, 2793 KiB  
Communication
Mechanical Properties Enhancement of the Au-Cu-Al Alloys via Phase Constitution Manipulation
by Kang-Wei Goo, Wan-Ting Chiu, Ayano Toriyabe, Masahiro Homma, Akira Umise, Masaki Tahara, Kenji Goto, Takumi Sannomiya and Hideki Hosoda
Materials 2021, 14(11), 3122; https://doi.org/10.3390/ma14113122 - 7 Jun 2021
Cited by 1 | Viewed by 2482
Abstract
To enhance the mechanical properties (e.g., strength and elongation) of the face-centered cubic (fcc) α-phase in the Au-Cu-Al system, this study focused on the introduction of the martensite phase (doubled B19 (DB19) crystal structure of Au2CuAl) via the manipulation of alloy [...] Read more.
To enhance the mechanical properties (e.g., strength and elongation) of the face-centered cubic (fcc) α-phase in the Au-Cu-Al system, this study focused on the introduction of the martensite phase (doubled B19 (DB19) crystal structure of Au2CuAl) via the manipulation of alloy compositions. Fundamental evaluations, such as microstructure observations, phase identifications, thermal analysis, tensile behavior examinations, and reflectance analysis, have been conducted. The presence of fcc annealing twins was observed in both the optical microscope (OM) and the scanning electron microscope (SEM) images. Both strength and elongation of the alloys were greatly promoted while the DB19 martensite phase was introduced into the alloys. Amongst all the prepared specimens, the 47Au41Cu12Al and the 44Au44Cu12Al alloys performed the optimized mechanical properties. The enhancement of strength and ductility in these two alloys was achieved while the stress plateau was observed during the tensile deformation. A plot of the ultimate tensile strength (UTS) against fracture strain was constructed to illustrate the effects of the introduction of the DB19 martensite phase on the mechanical properties of the alloys. Regardless of the manipulation of the alloy compositions and the introduction of the DB19 martensite phase, the reflectance stayed almost identical to pure Au. Full article
(This article belongs to the Special Issue Structure and Mechanical Properties of Alloys)
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<p>OM images of (<b>a</b>) 57Au31Cu12Al, (<b>b</b>) 55Au33Cu12Al, (<b>c</b>) 47Au41Cu12Al, and (<b>d</b>) 44Au44Cu12Al alloys as well as SEM images of (<b>e</b>) 57Au31Cu12Al and the (<b>f</b>) 44Au44Cu12Al alloys.</p>
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<p>X-ray diffraction patterns of (<b>a</b>) 57Au31Cu12Al, (<b>b</b>) 55Au33Cu12Al, (<b>c</b>) 47Au41Cu12Al, and (<b>d</b>) 44Au44Cu12Al alloys at 293 K (±3 K). (The subscript of α indicates the α-phase and the subscript of M suggests the DB19 martensite phase).</p>
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<p>DSC curves of (<b>a</b>) 57Au31Cu12Al, (<b>b</b>) 55Au33Cu12Al, (<b>c</b>) 47Au41Cu12Al, and (<b>d</b>) 44Au44Cu12Al alloys. The inserted figures indicate the enlarged transformation peaks. <span class="html-italic">A</span><sub>s</sub>, <span class="html-italic">A</span><sub>f</sub>, <span class="html-italic">M</span><sub>s</sub>, and <span class="html-italic">M</span><sub>f</sub> indicate the austenite (reverse martensite) transformation start temperature, austenite transformation finish temperature, martensite transformation start temperature, and martensite transformation finish temperature, respectively.</p>
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<p>Stress–strain curves of the tensile tests of (<b>a</b>) 57Au31Cu12Al, (<b>b</b>) 55Au33Cu12Al, (<b>c</b>) 47Au41Cu12Al, and (<b>d</b>) 44Au44Cu12Al alloys at 293 K (±3 K). The cross symbols indicate the fracture of the specimens.</p>
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<p>The relationship between the UTS and the fraction strain of 57Au31Cu12Al, 55Au33Cu12Al, 47Au41Cu12Al, and 44Au44Cu12Al alloys. (The α and M indicate the α-phase and the DB19 martensite phase, respectively).</p>
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<p>The cross-section SEM images and the zoomed-in images of (<b>a</b>,<b>c</b>) 55Au33Cu12Al and (<b>b</b>,<b>d</b>) 47Au41Cu12Al alloys.</p>
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<p>Reflectance analysis results of (<b>a</b>) 57Au31Cu12Al, (<b>b</b>) 55Au33Cu12Al, (<b>c</b>) 47Au41Cu12Al, and (<b>d</b>) 44Au44Cu12Al alloys as well as the (<b>e</b>) pure Au.</p>
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3 pages, 191 KiB  
Editorial
Editorial Materials: Special Issue on Advances in Luminescent Engineered Nanomaterials
by Luís Pinto da Silva
Materials 2021, 14(11), 3121; https://doi.org/10.3390/ma14113121 - 7 Jun 2021
Viewed by 1985
Abstract
Engineered nanomaterials are purposely manufactured particles with sizes typically between 1 and 100 nm, which can be either organic, inorganic, or organometallic in nature [...] Full article
(This article belongs to the Special Issue Advances in Luminescent Engineered Nanomaterials)
14 pages, 5650 KiB  
Article
Effect of Confining Conditions on the Hydraulic Conductivity Behavior of Fiber-Reinforced Lime Blended Semiarid Soil
by Abdullah Ali Shaker, Mosleh Ali Al-Shamrani, Arif Ali Baig Moghal and Kopparthi Venkata Vydehi
Materials 2021, 14(11), 3120; https://doi.org/10.3390/ma14113120 - 6 Jun 2021
Cited by 14 | Viewed by 3115
Abstract
The hydraulic properties of expansive soils are affected due to the formation of visible cracks in the dry state. Chemical stabilization coupled with fiber reinforcement is often considered an effective strategy to improve the geotechnical performance of such soils. In this study, hydraulic [...] Read more.
The hydraulic properties of expansive soils are affected due to the formation of visible cracks in the dry state. Chemical stabilization coupled with fiber reinforcement is often considered an effective strategy to improve the geotechnical performance of such soils. In this study, hydraulic conductivity tests have been conducted on expansive clay using two different types of fibers (fiber cast (FC) and fiber mesh (FM)) exhibiting different surface morphological properties. The fiber parameters include their dosage (added at 0.2% to 0.6% by dry weight of soil) and length (6 and 12 mm). Commercially available lime is added to ensure proper bonding between clay particles and fiber materials, and its dosage was fixed at 6% (by dry weight of the soil). Saturated hydraulic conductivity tests were conducted relying on a flexible wall permeameter on lime-treated fiber-blended soil specimens cured for 7 and 28 days. The confining pressures were varied from 50 to 400 kPa, and the saturated hydraulic conductivity values (ksat) were determined. For FC fibers, an increase in fiber dosage caused ksat values to increase by 9.5% and 94.3% for the 6 and 12 mm lengths, respectively, at all confining pressures and curing periods. For FM fibers, ksat values for samples mixed with 6 mm fiber increased by 12 and 99.2% for 6 and 12 mm lengths, respectively for all confining pressures at the end of the 28-day curing period. The results obtained from a flexible wall permeameter (FWP) were compared with those of a rigid wall permeameter (RWP) available in the literature, and the fundamental mechanism responsible for such variations is explained. Full article
(This article belongs to the Special Issue Testing of Materials and Elements in Civil Engineering (2nd Edition))
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<p>Fibers used in the study.</p>
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<p>Schematic diagram of a flexible wall constant head permeameter.</p>
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<p>Variations in saturated hydraulic conductivity (k<sub>sat</sub>) with confining pressure (<b>a</b>) FC (<b>b</b>) FM without lime treatment (without curing).</p>
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<p>Variations in saturated hydraulic conductivity (k<sub>sat</sub>) with confining pressure (<b>a</b>) FC (<b>b</b>) FM with lime treatment (without curing).</p>
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<p>Variations in saturated hydraulic conductivity (k<sub>sat</sub>) with confining pressure (<b>a</b>) FC (<b>b</b>) FM with lime treatment (after 7-day curing period).</p>
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<p>Variation of saturated hydraulic conductivity with confining pressure (<b>a</b>) FC (<b>b</b>) FM with lime treatment (after 28-day curing period).</p>
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<p>Variation of saturated hydraulic conductivity with lime content and confining pressure (<b>a</b>) 0.2%, 6mm; (<b>b</b>) 0.2%, 12mm; (<b>c</b>) 0.6%, 6mm; (<b>d</b>) 0.6%, 12mm.</p>
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<p>Variation of saturated hydraulic conductivity with lime content and confining pressure (<b>a</b>) 0.2%, 6mm; (<b>b</b>) 0.2%, 12mm; (<b>c</b>) 0.6%, 6mm; (<b>d</b>) 0.6%, 12mm.</p>
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<p>Variation of k<sub>sat</sub> values with curing period and confining pressure (<b>a</b>) FC_0.2% (<b>b</b>) FC_0.6% (<b>c</b>) FM_0.2% (<b>d</b>) FM_0.6%.</p>
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<p>Variation of k<sub>sat</sub> values with curing period and confining pressure (<b>a</b>) FC_0.2% (<b>b</b>) FC_0.6% (<b>c</b>) FM_0.2% (<b>d</b>) FM_0.6%.</p>
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<p>Comparison of hydraulic conductivity values from FWP and RWP (0-day curing period).</p>
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<p>Comparison of hydraulic conductivity values from FWP and RWP (7-day curing period).</p>
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<p>Comparison of hydraulic conductivity values from FWP and RWP (28-day curing period).</p>
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18 pages, 8383 KiB  
Article
Strengthening of Continuous Reinforced Concrete Deep Beams with Large Openings Using CFRP Strips
by Mohammed Riyadh Khalaf, Ali Hussein Ali Al-Ahmed, Abbas AbdulMajeed Allawi and Ayman El-Zohairy
Materials 2021, 14(11), 3119; https://doi.org/10.3390/ma14113119 - 6 Jun 2021
Cited by 9 | Viewed by 3019
Abstract
To accommodate utilities in buildings, different sizes of openings are provided in the web of reinforced concrete deep beams, which cause reductions in the beam strength and stiffness. This paper aims to investigate experimentally and numerically the effectiveness of using carbon fiber reinforced [...] Read more.
To accommodate utilities in buildings, different sizes of openings are provided in the web of reinforced concrete deep beams, which cause reductions in the beam strength and stiffness. This paper aims to investigate experimentally and numerically the effectiveness of using carbon fiber reinforced polymer (CFRP) strips, as a strengthening technique, to externally strengthen reinforced concrete continuous deep beams (RCCDBs) with large openings. The experimental work included testing three RCCDBs under five-point bending. A reference specimen was prepared without openings to explore the reductions in strength and stiffness after providing large openings. Openings were created symmetrically at the center of spans of the other specimens to represent 40% of the overall beam depth. Moreover, finite elements (FE) analysis was validated using the experimental results to conduct a parametric study on RCCDBs strengthened with CFRP strips. The results confirmed reductions in the ultimate load by 21% and 7% for the un-strengthened and strengthened specimens, respectively, due to the large openings. Although the large openings caused reductions in capacities, the CFRP strips limited the deterioration by enhancing the specimen capacity by 17% relative to the un-strengthened one. Full article
(This article belongs to the Special Issue Fiber Reinforced Materials for Buildings Strengthening)
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<p>Illustration of a reinforced concrete continuous deep beam.</p>
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<p>Typical layouts of the tested specimens (<b>a</b>) RCCDBs without openings; (<b>b</b>) RCCDBs with openings (all dimensions are in mm).</p>
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<p>Details of steel reinforcement for the tested specimens: (<b>a</b>) specimen CDB–Solid; (<b>b</b>) specimens CDB–O–U and CDB–O–S (all dimensions are in mm).</p>
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<p>Illustration of the strengthening scheme with CFRP strips around openings of specimen CDB–O–S (all dimensions are in mm).</p>
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<p>Test setup.</p>
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<p>Modes of failure for the tested specimens. (<b>a</b>) Specimen CDB–Solid; (<b>b</b>) Specimen CDB–O–U; (<b>c</b>) Specimen CDB–O–S.</p>
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<p>Load mid-span deflection curves for the tested specimens.</p>
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<p>Concrete uniaxial compressive and tensile stress–strain curves. (<b>a</b>) In compression; (<b>b</b>) in tension.</p>
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<p>FE mesh and discretization.</p>
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<p>Load mid-span deflection curves for the experimental and FE results. (<b>a</b>) Specimen CDB–Solid; (<b>b</b>) specimen CDB–O–U; (<b>c</b>) specimen CDB–O–S.</p>
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<p>Crack patterns of the tested specimens in experimental setup and ABAQUS. (<b>a</b>) Specimen CDB–Solid; (<b>b</b>) specimen CDB–O–U; (<b>c</b>) specimen CDB–O–S.</p>
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<p>Crack patterns of the tested specimens in experimental setup and ABAQUS. (<b>a</b>) Specimen CDB–Solid; (<b>b</b>) specimen CDB–O–U; (<b>c</b>) specimen CDB–O–S.</p>
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<p>Typical layouts of the RCCDBs with different ratios of the opening dimensions (all dimensions are in mm): (<b>a</b>) ratio: 1.5; (<b>b</b>) ratio: 2.0.</p>
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<p>Effect of the ratio of the opening dimensions on the behavior of RCCDBs. (<b>a</b>) Un-strengthened beams; (<b>b</b>) strengthened beams.</p>
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<p>Effectiveness of CFRP strips on strengthening RCCDBs with different ratios of the opening dimensions. (<b>a</b>) Opening ratio of 1.0; (<b>b</b>) opening ratio of 1.5; (<b>c</b>) opening ratio of 2.</p>
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<p>Effectiveness of CFRP strips on strengthening RCCDBs with different ratios of the opening dimensions. (<b>a</b>) Opening ratio of 1.0; (<b>b</b>) opening ratio of 1.5; (<b>c</b>) opening ratio of 2.</p>
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<p>Effect of ratios of the opening dimensions on the FE crack patterns for the un-strengthened RCCDBs. (<b>a</b>) CDB–O–U-R1.0; (<b>b</b>) CDB–O–U-R1.5; (<b>c</b>) CDB–O–U-R2.0.</p>
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<p>Effect of ratios of the opening dimensions on the FE crack pattern for the strengthened RCCDBs. (<b>a</b>) CDB–O–S-R1.0; (<b>b</b>) CDB–O–S-R1.5; (<b>c</b>) CDB–O–S-R2.0.</p>
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<p>Typical layout of the RCCDBs with openings to consider the load distribution factor.</p>
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<p>Effect of the load distribution factor on load–mid-span-deflection relationships of RCCDBs without openings (solid).</p>
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<p>Effect of the load distribution factor on load–mid-span-deflection relationships of the un-strengthened RCCDBs with different ratios of the opening dimensions. (<b>a</b>) Opening ratio of 1.0; (<b>b</b>) opening ratio of 1.5; (<b>c</b>) opening ratio of 2.0.</p>
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<p>Effect of the load distribution factor on load–mid-span-deflection relationships of the strengthened RCCDBs with different ratios of the opening dimensions. (<b>a</b>) Opening ratio of 1.0; (<b>b</b>) opening ratio of 1.5; (<b>c</b>) opening ratio of 2.0.</p>
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<p>Effect of the load distribution factor on load–mid-span-deflection relationships of the strengthened RCCDBs with different ratios of the opening dimensions. (<b>a</b>) Opening ratio of 1.0; (<b>b</b>) opening ratio of 1.5; (<b>c</b>) opening ratio of 2.0.</p>
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13 pages, 9703 KiB  
Article
Air Permeability of Maraging Steel Cellular Parts Made by Selective Laser Melting
by Annadurai Dhinakar, Bai-En Li, Yo-Cheng Chang, Kuo-Chi Chiu and Jhewn-Kuang Chen
Materials 2021, 14(11), 3118; https://doi.org/10.3390/ma14113118 - 6 Jun 2021
Cited by 6 | Viewed by 2553
Abstract
Additive manufacturing, such as selective laser melting (SLM), can be used to manufacture cellular parts. In this study, cellular coupons of maraging steels are prepared through SLM by varying hatch distance. Air flow and permeability of porous maraging steel blocks are obtained for [...] Read more.
Additive manufacturing, such as selective laser melting (SLM), can be used to manufacture cellular parts. In this study, cellular coupons of maraging steels are prepared through SLM by varying hatch distance. Air flow and permeability of porous maraging steel blocks are obtained for samples of different thickness based on the Darcy equation. By reducing hatch distance from 0.75 to 0.4 mm, the permeability decreases from 1.664 × 10−6 mm2 to 0.991 × 10−6 mm2 for 4 mm thick coupons. In addition, by increasing the thickness from 2 to 8 mm, the permeability increases from 0.741 × 10−6 mm2 to 1.345 × 10−6 mm2 at 16.2 J/mm3 energy density and 0.14 MPa inlet pressure. Simulation using ANSYS-Fluent is conducted to observe the pressure difference across the porous coupons and is compared with the experimental results. Surface artifacts and the actual morphology of scan lines can cause the simulated permeability to deviate from the experimental values. The measured permeability of maraging steel coupons is regression fit with both energy density and size of samples which provide a design guideline of porous mold inserts for industry applications such as injection molding. Full article
(This article belongs to the Special Issue Advances in Metal Additive Manufacturing)
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<p>SEM image of printed structures showing average 0.13 mm scan line width and 0.3 mm hatch distance (or D1 specimen in <a href="#materials-14-03118-t002" class="html-table">Table 2</a>).</p>
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<p>Schematics of the apparatus for air flow across cellular test coupons.</p>
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<p>CAD sample constructed using Solidworks for D5 sample.</p>
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<p>Compressed air flow through cellular coupons shown for D3 sample.</p>
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<p>Schematic view of flow field in simulation showing the pressure drop (left: gas inlet and right: gas outlet).</p>
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<p>Binary image showing projected pores (black parts) by surface grinding the (<b>a</b>) D1, (<b>b</b>) D2, (<b>c</b>) D3, (<b>d</b>) D4, (<b>e</b>) D5, (<b>f</b>) D6, (<b>g</b>) D7, (<b>h</b>) D8, and (<b>i</b>) D9 samples, respectively. (The width and length of each image corresponds to the surface area of 10 mm × 10 mm).</p>
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<p>CT images of pores changing with thickness of samples. Vertical direction corresponds to the thickness direction of the samples. The inset of 1~3 mm represents the thickness of the samples.</p>
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<p>Flow rate of air through porous coupons for variation in thickness and energy density when inlet pressure is 0.27 MPa.</p>
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<p>Change of air flow rate across the 4 mm cellular coupons made by different energy densities and tested at three inlet pressures.</p>
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<p>Relationship between air permeability and energy density for 4 mm thickness coupons tested at different inlet pressures.</p>
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<p>Permeability as a function of energy density (J/mm<sup>3</sup>) and coupon thickness at inlet pressure of 0.14 MPa.</p>
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<p>Relationship between permeability with number of layers obtain through simulation at inlet pressure 0.14 MPa.</p>
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<p>Comparison between permeability of cellular coupons obtained using experimental and simulation for (<b>a</b>) D3, (<b>b</b>) D5, (<b>c</b>) D7 and (<b>d</b>) D9 conditions at 0.14 MPa inlet pressure.</p>
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<p>Relationship between experimental energy density and porosity shown with regression equation.</p>
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<p>Comparison between fitted permeability and experimental permeability.</p>
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16 pages, 8058 KiB  
Article
On Characteristics of Ferritic Steel Determined during the Uniaxial Tensile Test
by Ihor Dzioba, Sebastian Lipiec, Robert Pala and Piotr Furmanczyk
Materials 2021, 14(11), 3117; https://doi.org/10.3390/ma14113117 - 6 Jun 2021
Cited by 13 | Viewed by 2522
Abstract
Tensile uniaxial test is typically used to determine the strength and plasticity of a material. Nominal (engineering) stress-strain relationship is suitable for determining properties when elastic strain dominates (e.g., yield strength, Young’s modulus). For loading conditions where plastic deformation is significant (in front [...] Read more.
Tensile uniaxial test is typically used to determine the strength and plasticity of a material. Nominal (engineering) stress-strain relationship is suitable for determining properties when elastic strain dominates (e.g., yield strength, Young’s modulus). For loading conditions where plastic deformation is significant (in front of a crack tip or in a neck), the use of true stress and strain values and the relationship between them are required. Under these conditions, the dependence between the true values of stresses and strains should be treated as a characteristic—a constitutive relationship of the material. This article presents several methodologies to develop a constitutive relationship for S355 steel from tensile test data. The constitutive relationship developed was incorporated into a finite element analysis of the tension test and verified with the measured tensile test data. The method of the constitutive relationship defining takes into account the impact of high plastic strain, the triaxiality stress factor, Lode coefficient, and material weakness due to the formation of microvoids, which leads to obtained correctly results by FEM (finite elements method) calculation. The different variants of constitutive relationships were applied to the FEM loading simulation of the three-point bending SENB (single edge notched bend) specimen to evaluate their applicability to the calculation of mechanical fields in the presence of a crack. Full article
(This article belongs to the Special Issue Testing of Materials and Elements in Civil Engineering (2nd Edition))
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<p>Steel S355 of ferrite-perlite (<span class="html-italic">FP</span>) microstructure: (<b>a</b>) ×1000; (<b>b</b>) ×5000.</p>
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<p>The stress-strain plots for specimens of S355 steel: (<b>a</b>) nominal values; (<b>b</b>) true values.</p>
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<p>Deformed microstructure of S355 steel at different distance from the fracture plane: (<b>a</b>) 17 mm (undeformed material); (<b>b</b>) 7 mm; (<b>c</b>) 4 mm; (<b>d</b>) 2 mm; and (<b>e</b>,<b>f</b>) 0.1–0.2 mm.</p>
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<p>Deformed microstructure of S355 steel at different distance from the fracture plane: (<b>a</b>) 17 mm (undeformed material); (<b>b</b>) 7 mm; (<b>c</b>) 4 mm; (<b>d</b>) 2 mm; and (<b>e</b>,<b>f</b>) 0.1–0.2 mm.</p>
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<p>Histograms and graphs for normal distributions of grain length at different distances from the fracture plane of the specimen: (<b>a</b>) 17 mm; (<b>b</b>) 10 mm; (<b>c</b>) 5 mm; (<b>d</b>) 3 mm; (<b>e</b>) 2 mm; and (<b>f</b>) 0.1 mm.</p>
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<p>Graphs of changes in ferrite grain length (<b>a</b>) and strain level (<b>b</b>) in a uniaxially tensile specimen made of S355 steel.</p>
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<p>The scheme presents the measurement of strain in a uniaxial tensile test of the specimen (in the photo) and the obtained strain values together with the fitting function.</p>
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<p>Examples of forming neck during specimen tensile (recorded by video-camera Olympus): (<b>a</b>) ~250 s, start of necking; (<b>b</b>) ~350 s; and (<b>c</b>) ~450 s, before specimen fracture.</p>
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<p>(<b>a</b>) Reduction in the specimen cross-sectional area S and increase in stresses <span class="html-italic">σ</span><sub>a</sub> during loading; (<b>b</b>) the stress-strain plots for nominal and true values.</p>
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<p>(<b>a</b>) The graphs of nominal stresses, potential increase, and minimum specimen cross-section during the tensile test; (<b>b</b>) the graphs of nominal and true stresses as a function of nominal strain.</p>
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<p>Numerical model of the tensile specimen (<b>a</b>); undeformed mesh fragment near blocked plane (<b>b</b>); deformed mesh fragment near blocked plane (<b>c</b>).</p>
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<p>Numerical model of SENB specimen: (<b>a</b>) scheme of the boundary conditions; (<b>b</b>) scheme of the mesh.</p>
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<p>The stress-strain graphs for: (<b>a</b>) var. 1, (<b>b</b>) var. 2, (<b>c</b>) var. 3, and suitable numerical and experimental force-elongation curves for: (<b>d</b>) var. 1, (<b>e</b>) var. 2, and (<b>f</b>) var. 3.</p>
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<p>View of break surface of the tensile specimen (<b>a</b>) and a scheme of the break plane profile (<b>b</b>).</p>
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<p>The distributions of plastic strains (<b>a</b>) and of stress components (<b>b</b>–<b>d</b>) in front of the crack calculated by means of FEM.</p>
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<p>Development of voids in a uniaxially tensile specimen: (<b>a</b>) ~1.0 mm since the fracture plane; (<b>b</b>) directly at the fracture plane.</p>
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<p>Deformed and damaged material in front of crack tip in SENB specimen: (<b>a</b>) S355 steel; (<b>b</b>) 14MoV6 steel.</p>
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21 pages, 17160 KiB  
Article
Effect of Fire Temperature and Exposure Time on High-Strength Steel Bolts Microstructure and Residual Mechanical Properties
by Paweł Artur Król and Marcin Wachowski
Materials 2021, 14(11), 3116; https://doi.org/10.3390/ma14113116 - 6 Jun 2021
Cited by 4 | Viewed by 2909
Abstract
In this study, the influence of different fire conditions on tempered 32CrB3 steel bolts of Grade 8.8 was investigated. In this research different temperatures, heating time, and cooling methods were correlated with the microstructure, hardness, and residual strength of the bolts. Chosen parameters [...] Read more.
In this study, the influence of different fire conditions on tempered 32CrB3 steel bolts of Grade 8.8 was investigated. In this research different temperatures, heating time, and cooling methods were correlated with the microstructure, hardness, and residual strength of the bolts. Chosen parameters of heat treatments correspond to simulated natural fire conditions that may occur in public facilities. Heat treated and unheated samples cut out from a series of tested bolts were subjected to microstructural tests using light microscopy (LM), scanning electron microscopy (SEM), energy dispersive spectroscopy (EDS), XRD phase analysis, and the quantitative analysis of the microstructure. The results of the microstructure tests were compared with the results of strength tests, including hardness and the ultimate residual tensile strength of the material (UTS) in the initial state and after the heat treatments. Results of the investigations revealed considerable microstructural changes in the bolt material as a result of exposing it to different fire conditions and cooling methods. A conducted comparative analysis also showed a significant effect of all such factors as the temperature level of the simulated fire, its duration, and the fire-fighting method on the mechanical properties of the bolts. Full article
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<p>Diagram presenting dependence of microstructural indices, i.e., mean equivalent diameters of ferrite and pearlite grains, HV hardness, and ultimate tensile strength (UTS) on heat treatment parameters.</p>
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<p>Diagram of correlations between hardness HV and residual tensile strength of the bolt steel after secondary heat treatment depending on parameters of this treatment.</p>
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<p>Diagram of dependencies between bolt steel hardness and bolt residual tensile strength on heating time for samples: (<b>a</b>) naturally air-cooled; (<b>b</b>) shock water-cooled.</p>
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<p>Diagram of dependencies between bolt steel hardness and bolt residual tensile strength on heating time for samples subjected to secondary heat treatment for the time of: (<b>a</b>) 60 min; (<b>b</b>) 240 min.</p>
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17 pages, 3666 KiB  
Article
Comparison of Mechanical Properties of Chairside CAD/CAM Restorations Fabricated Using a Standardization Method
by Myung-Sik Hong, Yu-Sung Choi, Hae-Hyoung Lee, Jung-Hwan Lee and Junyong Ahn
Materials 2021, 14(11), 3115; https://doi.org/10.3390/ma14113115 - 6 Jun 2021
Cited by 7 | Viewed by 2668
Abstract
The aim of this in vitro study was to investigate the fracture resistance, fracture failure pattern, and fractography of four types of chairside computer-aided design/computer-aided manufacturing (CAD/CAM) restoration materials in teeth and titanium abutments fabricated using a standardization method. An artificial mandibular left [...] Read more.
The aim of this in vitro study was to investigate the fracture resistance, fracture failure pattern, and fractography of four types of chairside computer-aided design/computer-aided manufacturing (CAD/CAM) restoration materials in teeth and titanium abutments fabricated using a standardization method. An artificial mandibular left first premolar prepared for all-ceramic crown restoration was scanned. Forty extracted mandibular molars and cylindrical titanium specimens were milled into a standardized shape. A total of eighty CAD/CAM restoration blocks were milled into a crown and twenty pieces of each lithium disilicate (LS), polymer-infiltrated-ceramic-network (PICN), resin nano ceramic (RNC), and zirconia-reinforced lithium silicate (ZLS) materials were used. Crowns were bonded to abutments, and all specimens underwent thermal cycling treatment for 10,000 cycles. Fracture resistance was measured using a universal testing machine and fracture failure patterns were analyzed using optical microscopy and scanning electron microscopy. Statistical differences were analyzed using appropriate ANOVA, Tukey HSD post hoc tests, and independent sample t-tests (α = 0.05). The results indicated that, in both teeth abutments and titanium abutments, the fracture resistances showed significantly the highest values in LS and the second highest in ZLS (p < 0.05). The fracture resistances based on teeth abutments and titanium abutments were significantly different in all the CAD/CAM restoration materials (p < 0.05). There are statistically significant correlations between the types of materials and the types of abutments (p < 0.05). Each of the different materials showed different fracture failure patterns, and there was no noticeable difference in fractographic analysis. Lithium disilicates and zirconia-reinforced lithium silicates exhibited statistically high fracture resistance, indicating their suitability as restoration materials for natural teeth or implant abutments. There were no distinct differences in the fracture pattern based on the restoration and abutment materials showed that the fracture initiated at the groove where the ball indenter was toughed and propagated toward the axial wall. Full article
(This article belongs to the Special Issue Advances in Dental Materials)
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Figure 1
<p>Standardization of tooth abutment: (<b>A</b>):VITA CAD-Temp multiColor block (left); schematic diagram for cutting block (right). (<b>B</b>): Mandibular premolar tooth (left); block with tooth placed inside (right). (<b>C</b>): The STL file of prepared teeth for standardization. (<b>D</b>): Tooth abutment fabricated using milling machine. (<b>E</b>): Standardized tooth abutments. (<b>F</b>): The STL file of the crown shape for standardization. (<b>G</b>): Specimen with crown cemented to tooth abutments. STL, standard tessellation language.</p>
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<p>Standardization of tooth abutment: (<b>A</b>):VITA CAD-Temp multiColor block (left); schematic diagram for cutting block (right). (<b>B</b>): Mandibular premolar tooth (left); block with tooth placed inside (right). (<b>C</b>): The STL file of prepared teeth for standardization. (<b>D</b>): Tooth abutment fabricated using milling machine. (<b>E</b>): Standardized tooth abutments. (<b>F</b>): The STL file of the crown shape for standardization. (<b>G</b>): Specimen with crown cemented to tooth abutments. STL, standard tessellation language.</p>
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<p>Means and standard deviations of fracture resistance. (<b>A</b>): Tooth abutment. (<b>B</b>): Titanium abutment. Same alphabet letters indicate no significant differences at <span class="html-italic">p</span> &lt; 0.05. LS, lithium disilicate; PICN, polymer-infiltrated-ceramic-network; RNC, resin nano ceramic; ZLS, zirconia-reinforced lithium silicate; TO, tooth abutment; TI, titanium abutment.</p>
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<p>Means and standard deviations of fracture resistance. * Denotes significant differences at <span class="html-italic">p</span> &lt; 0.05. LS, lithium disilicate; PICN, polymer-infiltrated-ceramic-network; RNC, resin nano ceramic; ZLS, zirconia-reinforced lithium silicate; TO, tooth abutment; TI, titanium abutment.</p>
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<p>Crown failure mode (<b>A</b>): Tooth abutment. (<b>B</b>): Titanium abutment. LS, lithium disilicate; PICN, polymer-infiltrated-ceramic-network; RNC, resin nano ceramic; ZLS, zirconia-reinforced lithium silicate; TO, tooth abutment; TI, titanium abutment.</p>
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<p>Fracture failure patterns in tooth and titanium abutments (<b>A</b>): PICN_TO specimen showing mixed failure pattern. (<b>B</b>): LS_TO specimen showing adhesive failure pattern. (<b>C</b>): LS_TI specimen showing mixed failure pattern. (<b>D</b>): RNC_TI specimen showing an adhesive failure pattern; the cement was attached to the abutment. (<b>E</b>): ZLS_TI specimen showing an adhesive failure pattern; the cement was attached to the crown fragment. PICN, polymer-infiltrated-ceramic-network; TO, tooth abutment; LS, lithium disilicate; TI, titanium abutment; RNC, resin nano ceramic; ZLS, zirconia-reinforced lithium silicate; C, cement; To, tooth; Ti, titanium.</p>
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<p>Fracture failure patterns in tooth and titanium abutments (<b>A</b>): PICN_TO specimen showing mixed failure pattern. (<b>B</b>): LS_TO specimen showing adhesive failure pattern. (<b>C</b>): LS_TI specimen showing mixed failure pattern. (<b>D</b>): RNC_TI specimen showing an adhesive failure pattern; the cement was attached to the abutment. (<b>E</b>): ZLS_TI specimen showing an adhesive failure pattern; the cement was attached to the crown fragment. PICN, polymer-infiltrated-ceramic-network; TO, tooth abutment; LS, lithium disilicate; TI, titanium abutment; RNC, resin nano ceramic; ZLS, zirconia-reinforced lithium silicate; C, cement; To, tooth; Ti, titanium.</p>
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<p>Stereomicroscopy images (25× magnification) of crowns corresponding to the load area (<b>A</b>): features of crown fracture of the representative crown from the PICN_TO group. (<b>B</b>): Features of crown fracture of the representative crown from the RNC_TO group. (<b>C</b>): Features of crown fracture of the representative crown from the ZLS_TO group. (<b>D</b>): Features of crown fracture of the representative crown from the LS_TO group. (<b>E</b>): Features of crown fracture of the representative crown from the PICN_TI group. (<b>F</b>) Features of crown fracture of the representative crown from the RNC_TI group. (<b>G</b>): Features of crown fracture of the representative crown from the ZLS_TI group. (<b>H</b>): Features of crown fracture of the representative crown from the LS_TI group. Blue arrows indicate the load areas; red arrows refer to the directions of the crack propagations. PICN, polymer-infiltrated-ceramic-network; TO, tooth abutment; RNC, resin nano ceramic; ZLS, zirconia-reinforced lithium silicate; LS, lithium disilicate; TI, titanium abutment.</p>
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<p>Stereomicroscopy images (25× magnification) of crowns corresponding to the load area (<b>A</b>): features of crown fracture of the representative crown from the PICN_TO group. (<b>B</b>): Features of crown fracture of the representative crown from the RNC_TO group. (<b>C</b>): Features of crown fracture of the representative crown from the ZLS_TO group. (<b>D</b>): Features of crown fracture of the representative crown from the LS_TO group. (<b>E</b>): Features of crown fracture of the representative crown from the PICN_TI group. (<b>F</b>) Features of crown fracture of the representative crown from the RNC_TI group. (<b>G</b>): Features of crown fracture of the representative crown from the ZLS_TI group. (<b>H</b>): Features of crown fracture of the representative crown from the LS_TI group. Blue arrows indicate the load areas; red arrows refer to the directions of the crack propagations. PICN, polymer-infiltrated-ceramic-network; TO, tooth abutment; RNC, resin nano ceramic; ZLS, zirconia-reinforced lithium silicate; LS, lithium disilicate; TI, titanium abutment.</p>
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<p>SEM image of crowns in tooth and titanium abutments corresponding to the area of crack origin. (<b>A</b>): Representative crown from group LS_TO (50× magnification). (<b>B</b>): Representative crown from group PICN_TO (50× magnification). (<b>C</b>): Representative crown from group RNC_TO (33× magnification). (<b>D</b>): Representative crown from group ZLS_TO (100× magnification). (<b>E</b>): Representative crown from group LS_TI (50× magnification). (<b>F</b>): Representative crown from group PICN_TI (50× magnification). (<b>G</b>): Representative crown from group RNC_TI (336× magnification). (<b>H</b>): Representative crown from group ZLS_TI (43× magnification). Red arrows and circles indicate the origin; yellow arrows refer to the ‘fracture mirror’; blue arrows refer to the ‘hackle’.</p>
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14 pages, 5682 KiB  
Article
Al Matrix Composites Reinforced by Ti and C Dedicated to Work at Elevated Temperature
by Bartosz Hekner, Jerzy Myalski, Patryk Wrześniowski and Tomasz Maciąg
Materials 2021, 14(11), 3114; https://doi.org/10.3390/ma14113114 - 6 Jun 2021
Cited by 4 | Viewed by 2028
Abstract
In this paper, the applicability of aluminium matrix composites to high-temperature working conditions (not exceeding the Al melting point) was evaluated. The behaviour of Al-Ti-C composites at elevated temperatures was described based on microstructural and phase composition observations for composites heated at temperatures [...] Read more.
In this paper, the applicability of aluminium matrix composites to high-temperature working conditions (not exceeding the Al melting point) was evaluated. The behaviour of Al-Ti-C composites at elevated temperatures was described based on microstructural and phase composition observations for composites heated at temperatures of 540 and 600 °C over differing time intervals from 2 to 72 h. The materials investigated were aluminium matrix composites (AMC) reinforced with a spatial carbon (C) structure covered by a titanium (Ti) layer. This layer protected the carbon surface against contact with the aluminium during processing, protection which was maintained for the material’s lifetime and ensured the required phase compositions of Al4C3 phase limitation and AlTi3 phase creation. It was also proved that heat treatment influenced not only phase compositions but also the microstructure of the material, and, as a consequence, the properties of the composite. Full article
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<p>Phase diagram for (<b>a</b>) Ti-Al system [<a href="#B19-materials-14-03114" class="html-bibr">19</a>]; (<b>b</b>) Ti-C system [<a href="#B22-materials-14-03114" class="html-bibr">22</a>]; (<b>c</b>) Al-C system [<a href="#B23-materials-14-03114" class="html-bibr">23</a>]; L—liquid, G—gas, C—carbon.</p>
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<p>Microstructure of (<b>a</b>) spatial structure of PU foam; (<b>b</b>) Ti powder (SEM).</p>
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<p>Schematic diagram of processes performed.</p>
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<p>Free energy of formation in an Al-Ti-C (amorphous) system.</p>
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<p>Thermogravimetric analysis of an Al-Ti-C system (TG).</p>
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<p>Phase composition of Al-Ti-C system after thermogravimetric analyses at 1200 °C (XRD).</p>
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<p>The microstructure of the obtained reinforcement layers varied according to Ti particle suspension: (<b>a</b>) 10 vol.%; (<b>b</b>) 25 vol.%; (<b>c</b>) 40 vol.% in PF resin suspension. In insets, the cross-sections of foam are presented (SEM).</p>
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<p>The microstructure of composites obtained by infiltration of spatial structures with a range of Ti particle suspensions: (<b>a</b>) 5 vol.%; (<b>b</b>) 20 vol.%; (<b>c</b>) 40 vol.% used for Ti layer creation (SEM).</p>
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<p>(<b>a</b>) The microstructure and chemical distribution of (<b>b</b>) aluminium; (<b>c</b>) titanium; (<b>d</b>) carbon compounds in composite with layers created by a suspension of 20 vol.% of Ti (SEM + EDS).</p>
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<p>The microstructures of composites after heat treatment at 600 °C at varying times: (<b>a</b>) 2 h; (<b>b</b>) 8 h; (<b>c</b>) 24 h; (<b>d</b>) 72 h (SEM).</p>
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<p>Phase composition for AMC-Ti-C composite after heat treatment at 540 °C, over 8 and 72 h durations (XRD).</p>
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<p>Hardness and porosity of Al-Ti-C composites after heat treatment at different times (2–72 h) and temperatures (540 and 600 °C).</p>
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23 pages, 13434 KiB  
Article
Analysis of Deformation, the Stressed State and Fracture Predictions for Cogging Shafts with Convex Anvils
by Marcin Kukuryk
Materials 2021, 14(11), 3113; https://doi.org/10.3390/ma14113113 - 6 Jun 2021
Cited by 1 | Viewed by 2099
Abstract
In this article, a new manner of cogging a forging (type: shaft), consisting in the application of a two-stage process composed of preliminary shaping in convex anvils, and also principal forging in flat or shaped anvils, is presented. A new manner of forging [...] Read more.
In this article, a new manner of cogging a forging (type: shaft), consisting in the application of a two-stage process composed of preliminary shaping in convex anvils, and also principal forging in flat or shaped anvils, is presented. A new manner of forging brought about the formation of favorable conditions for achieving the maximum values of the effective strain in the central part of a forging, accompanied by a simultaneous absence of tensile stresses, which was exerting a favorable influence upon reforging the axial zone of an ingot. What was determined, was the effective geometric shapes of convex anvils; the efficiency of different technological parameters in the case of the intensity of reforging the axial zone of an ingot was analyzed as well. The investigations were complemented by means of predicting the formation of ductile fractures in the course of forging with the application of three different ductile fracture criteria. The comparison of theoretical and experimental outcomes of investigations indicates a good level of being commensurate. Full article
(This article belongs to the Special Issue Metal Forming and Forging)
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Figure 1
<p>Flow curve plots for specimens deformed at (<b>a</b>) constant strain rate of 1.0 s<sup>−1</sup> and different deformation temperatures and at (<b>b</b>) different strain rates and a constant temperature of 1273 K.</p>
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<p>Shape of anvils: (<b>a</b>) flat, (<b>b</b>) convex (angle: <span class="html-italic">α<sub>c</sub></span> = 135°, 150° and 165°), and (<b>c</b>) V-shaped (<span class="html-italic">α</span> = 140°), the numbers in the figure in mm.</p>
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<p>Schematic illustration of the cogging process: (<b>a</b>) finite element model for the forging experiment, (<b>b</b>) the hitting sequence on the ingot length (l/w<sub>d</sub> = 0.70; l/D<sub>0</sub> = 0.75), and (<b>c</b>) pass sequence for flat anvils (90° rotation).</p>
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<p>Schematic illustration of the cogging process: (<b>a</b>) finite element model for the forging experiment, (<b>b</b>) the hitting sequence on the ingot length (l/w<sub>d</sub> = 0.70; l/D<sub>0</sub> = 0.75), and (<b>c</b>) pass sequence for flat anvils (90° rotation).</p>
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<p>Order of forging the workpiece with convex anvils (<span class="html-italic">α<sub>c</sub></span> = 135°, 150°, and 165°), (<b>a</b>) after the first pass, (<b>b</b>) after the second pass.</p>
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<p>Order of forging the workpiece with a concave cross-section with flat anvils (<b>a</b>) after the first pass, (<b>b</b>) after the second pass.</p>
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<p>Order of forging the workpiece with a concave cross-section with V-shaped anvils (<b>a</b>) after the first pass, (<b>b</b>) after the second pass.</p>
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<p>Distribution of the effective strain (<b>a</b>), effective stress (<b>b</b>), mean stresses (<b>c</b>), and temperature (<b>d</b>) on the cross-section of the workpiece in the course of forging in convex anvils after the second pass (<span class="html-italic">α<sub>c</sub></span> = 135°, <span class="html-italic">ε<sub>c</sub></span> = 0.22).</p>
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<p>Distribution of the effective strain (<b>a</b>), effective stress (<b>b</b>), mean stresses (<b>c</b>), and temperature (<b>d</b>) on the cross-section of the workpiece in the course of forging in convex anvils after the second pass (<span class="html-italic">α<sub>c</sub></span> = 150°, <span class="html-italic">ε<sub>c</sub></span> = 0.22).</p>
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<p>Distribution of the effective strain (<b>a</b>), effective stress (<b>b</b>), mean stresses (<b>c</b>), and temperature (<b>d</b>) on the cross-section of the workpiece in the course of forging in convex anvils after the second pass (<span class="html-italic">α<sub>c</sub></span> = 150°, <span class="html-italic">ε<sub>c</sub></span> = 0.22).</p>
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<p>Distribution of the effective strain (<b>a</b>), effective stress (<b>b</b>), mean stresses (<b>c</b>), and temperature (<b>d</b>) on the cross-section of the workpiece in the course of forging in convex anvils after the second pass (<span class="html-italic">α<sub>c</sub></span> = 165°, <span class="html-italic">ε<sub>c</sub></span> = 0.22).</p>
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<p>Distribution of the effective strain (<b>a</b>), effective stress (<b>b</b>), mean stresses (<b>c</b>), and temperature (<b>d</b>) on the cross-section of the workpiece in the course of forging in convex anvils after the second pass (<span class="html-italic">α<sub>c</sub></span> = 135°, <span class="html-italic">ε<sub>c</sub></span> = 0.51).</p>
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<p>Distribution of the effective strain (<b>a</b>), effective stress (<b>b</b>), mean stresses (<b>c</b>), and temperature (<b>d</b>) on the cross-section of the workpiece in the course of forging in convex anvils after the second pass (<span class="html-italic">α<sub>c</sub></span> = 135°, <span class="html-italic">ε<sub>c</sub></span> = 0.51).</p>
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<p>Distribution of the effective strain (<b>a</b>), effective stress (<b>b</b>), mean stresses (<b>c</b>), and temperature (<b>d</b>) on the cross-section of the workpiece in the course of forging in convex anvils after the second pass (<span class="html-italic">α<sub>c</sub></span> = 150°, <span class="html-italic">ε<sub>c</sub></span> = 0.51).</p>
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<p>Distribution of the effective strain (<b>a</b>), effective stress (<b>b</b>), mean stresses (<b>c</b>), and temperature (<b>d</b>) on the cross-section of the workpiece in the course of forging in convex anvils after the second pass (<span class="html-italic">α<sub>c</sub></span> = 165°, <span class="html-italic">ε<sub>c</sub></span> = 0.51).</p>
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<p>Distribution of the effective strain (<b>a</b>), effective stress (<b>b</b>), mean stresses (<b>c</b>), and temperature (<b>d</b>) on the cross-section of the workpiece in the course of forging in convex anvils after the second pass (<span class="html-italic">α<sub>c</sub></span> = 165°, <span class="html-italic">ε<sub>c</sub></span> = 0.51).</p>
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<p>Influence of different angles of convex anvils <span class="html-italic">α<sub>c</sub></span> and reduction ratio <span class="html-italic">ε<sub>c</sub></span> on the effective strain <math display="inline"><semantics> <mover accent="true"> <mi>ε</mi> <mo>¯</mo> </mover> </semantics></math> (<b>a</b>) and the stress triaxiality ratio <span class="html-italic">T<sub>x</sub></span> (<b>b</b>) in the axial zone.</p>
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<p>Distribution of the effective strain (<b>a</b>), effective stress (<b>b</b>), mean stresses (<b>c</b>), and temperature (<b>d</b>) after the eighth pass of the forging with a concave cross-section in flat anvils (<span class="html-italic">α<sub>c</sub></span> = 150°, <span class="html-italic">ε<sub>c</sub></span> = 0.356, forging ratio 4.2).</p>
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<p>Distribution of the effective strain (<b>a</b>), effective stress (<b>b</b>), mean stresses (<b>c</b>), and temperature (<b>d</b>) after the fourth pass of the forging with a concave cross-section in V-shaped anvils (<span class="html-italic">α<sub>c</sub></span> = 150°, <span class="html-italic">ε<sub>c</sub></span> = 0.356, forging ratio 4.2).</p>
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<p>Distribution of the effective strain (<b>a</b>), effective stress (<b>b</b>), mean stresses (<b>c</b>), and temperature (<b>d</b>) after the fourth pass of the forging with a concave cross-section in V-shaped anvils (<span class="html-italic">α<sub>c</sub></span> = 165°, <span class="html-italic">ε<sub>c</sub></span> = 0.51, forging ratio 4.2).</p>
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<p>Influence of different passes upon the effective strain <math display="inline"><semantics> <mover accent="true"> <mi>ε</mi> <mo>¯</mo> </mover> </semantics></math> (<b>a</b>) and the stress triaxiality ratio Tx (b) in the axial zone in the course of the cogging in flat anvils of the forging with a concave cross-section for different angles and reduction ratio: 1—<span class="html-italic">ε<sub>c</sub></span> = 0.22, <span class="html-italic">α<sub>c</sub></span> = 135°; 2—<span class="html-italic">ε<sub>c</sub></span> = 0.51, <span class="html-italic">α<sub>c</sub></span> = 135°; 3—<span class="html-italic">ε<sub>c</sub></span> = 0.22, <span class="html-italic">α<sub>c</sub></span> = 165°; 4—<span class="html-italic">ε<sub>c</sub></span> = 0.51, <span class="html-italic">α<sub>c</sub></span> = 165°.</p>
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<p>Influence of different passes upon the effective strain <math display="inline"><semantics> <mover accent="true"> <mi>ε</mi> <mo>¯</mo> </mover> </semantics></math> (<b>a</b>) and the stress triaxiality ratio <span class="html-italic">T<sub>x</sub></span> (<b>b</b>) in the axial zone in the course of the cogging in V-shaped anvils of the forging with a concave cross-section for different angles and reduction ratio: 1—<span class="html-italic">ε<sub>c</sub></span> = 0.22, <span class="html-italic">α<sub>c</sub></span> = 135°; 2—<span class="html-italic">ε<sub>c</sub></span> = 0.51, <span class="html-italic">α<sub>c</sub></span> = 135°; 3—<span class="html-italic">ε<sub>c</sub></span> = 0.22, <span class="html-italic">α<sub>c</sub></span> = 165°; 4—<span class="html-italic">ε<sub>c</sub></span> = 0.51, <span class="html-italic">α<sub>c</sub></span> = 165°.</p>
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<p>Distribution of the damage factors: (<b>a</b>) Cockcroft and Latham, (<b>b</b>) Oyane et al., and (<b>c</b>) Brozzo et al. after eighth pass of the forging with a concave cross-section in flat anvils (α<sub>c</sub> = 150°, ε<sub>c</sub> = 0.356, forging ratio 4.2).</p>
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<p>Distribution of the damage factors: (<b>a</b>) Cockcroft and Latham, (<b>b</b>) Oyane et al., and (<b>c</b>) Brozzo et al. after fourth pass of the forging with a concave cross-section in V-shaped anvils (α<sub>c</sub> = 150°, ε<sub>c</sub> = 0.356, forging ratio 4.2).</p>
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<p>Influence exerted by of different passes upon the damage factors: Cockcroft and Latham (<span class="html-italic">Ψ<sub>C-L</sub></span>), Oyane et al. (<span class="html-italic">Ψ<sub>O</sub></span>), and Brozzo et al. (<span class="html-italic">Ψ<sub>B</sub></span>) in the axial zone in the course of cogging of the forging with a concave cross-section in flat anvils (<b>a</b>) and in V-shaped anvils (<b>b</b>) for different angles and reduction ratio: 1—<span class="html-italic">ε<sub>c</sub></span> = 0.22, <span class="html-italic">α<sub>c</sub></span> = 135°; 2—<span class="html-italic">ε<sub>c</sub></span> = 0.51, <span class="html-italic">α<sub>c</sub></span> = 135°; 3—<span class="html-italic">ε<sub>c</sub></span> = 0.22, <span class="html-italic">α<sub>c</sub></span> = 165°; 4—<span class="html-italic">ε<sub>c</sub></span> = 0.51, <span class="html-italic">α<sub>c</sub></span> = 165°.</p>
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<p>Comparison of the computed and the measured temperature during the cogging process of the X5CrNi18-10 steel forged in flat anvils, forging ratio 4.2.</p>
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<p>Shape of the anvils used in the laboratory experimentation: (<b>a</b>) convex (<span class="html-italic">α<sub>c</sub></span> = 135°), (<b>b</b>) V-shaped (<span class="html-italic">α</span> = 140° × 140°), and (<b>c</b>) flat.</p>
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<p>Comparisons of the numerical (<b>A</b>) and experimental (<b>B</b>) distribution of effective strain on the cross-section surfaces of the X5CrNi18-10 steel specimens deformed in anvils: (<b>a</b>) convex (<span class="html-italic">α<sub>c</sub></span> = 135°, <span class="html-italic">ε<sub>c</sub></span> = 0.693), (<b>b</b>) V-shaped (<span class="html-italic">α</span> = 140° × 140°, <span class="html-italic">ε<sub>h</sub></span> = 0.35), and (<b>c</b>) flat (<span class="html-italic">ε<sub>h</sub></span> = 0.35).</p>
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11 pages, 6251 KiB  
Article
An Investigation on Spray-Granulated, Macroporous, Bioactive Glass Microspheres for a Controlled Drug Delivery System
by Henni Setia Ningsih, Liu-Gu Chen, Ren-Jei Chung and Yu-Jen Chou
Materials 2021, 14(11), 3112; https://doi.org/10.3390/ma14113112 - 6 Jun 2021
Cited by 4 | Viewed by 2672
Abstract
Bioactive glass (BG) has been regarded as an excellent candidate for biomedical applications due to its superior properties of bioactivity, biocompatibility, osteoconductivity and biodegradability. Thus, in this study, we aimed to fabricate drug carriers that were capable of loading therapeutic antibiotics while promoting [...] Read more.
Bioactive glass (BG) has been regarded as an excellent candidate for biomedical applications due to its superior properties of bioactivity, biocompatibility, osteoconductivity and biodegradability. Thus, in this study, we aimed to fabricate drug carriers that were capable of loading therapeutic antibiotics while promoting bone regeneration using macroporous BG microspheres, prepared by a spray drying method. Characterizations of particle morphology and specific surface area were carried out via scanning electron microscopy and nitrogen adsorption/desorption isotherm. Evaluations of in vitro bioactivity were performed based on Kokubo’s simulated body fluid to confirm the formation of the hydroxyapatite (HA) layer after immersion. In addition, the in vitro drug release behaviors were examined, using tetracycline as the therapeutic antibiotic in pH 7.4 and 5.0 environments. Finally, the results showed that BG microspheres of up to 33 μm could be mass-produced, targeting various therapeutic situations and their resulting bioactivities and drug release behaviors, and related properties were discussed. Full article
(This article belongs to the Special Issue Advances in Bioactive Materials)
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<p>SEM images of BG microspheres treated with (<b>a</b>) 0, (<b>b</b>) 5, (<b>c</b>) 10 and (<b>d</b>) 20 wt.% PMMA, with insets of their cross-sectional images.</p>
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<p>Histograms of sphere size distributions of (<b>a</b>) 0, (<b>b</b>) 5, (<b>c</b>) 10 and (<b>d</b>) 20 wt.% PMMA-treated BG microspheres.</p>
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<p>SEM images of BG microspheres treated with (<b>a</b>) 0, (<b>b</b>) 5, (<b>c</b>) 10 and (<b>d</b>) 20 wt.% PMMA after SBF immersion for 168 h.</p>
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<p>FTIR spectra of BG microspheres treated with 0, 5, 10 and 20 wt.% PMMA (<b>a</b>) before and (<b>b</b>) after SBF immersion for 168 h.</p>
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<p>Computed I<sub>1</sub>/I<sub>2</sub> intensity of 0, 5, 10 and 20 wt.% PMMA–treated BG microspheres before and after SBF immersion.</p>
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<p>Cumulative tetracycline release profiles of 0, 5, 10 and 20 wt.% PMMA-treated BG microspheres in (<b>a</b>) pH 7.4 and (<b>b</b>) pH 5.0 PBS solution at 37 °C.</p>
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<p>Cumulative tetracycline release profiles of gelatin-capsulated 0, 5, 10 and 20 wt.% PMMA-treated BG microspheres in (<b>a</b>) pH 7.4 and (<b>b</b>) pH 5.0 PBS solution at 37 °C.</p>
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<p>Schematic diagram of the formation mechanism of the PMMA-treated, granulated BG microspheres.</p>
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16 pages, 3410 KiB  
Article
Mechanical and Physicochemical Properties of 3D-Printed Agave Fibers/Poly(lactic) Acid Biocomposites
by Valeria Figueroa-Velarde, Tania Diaz-Vidal, Erick Omar Cisneros-López, Jorge Ramón Robledo-Ortiz, Edgar J. López-Naranjo, Pedro Ortega-Gudiño and Luis Carlos Rosales-Rivera
Materials 2021, 14(11), 3111; https://doi.org/10.3390/ma14113111 - 5 Jun 2021
Cited by 24 | Viewed by 3130
Abstract
In order to provide a second economic life to agave fibers, an important waste material from the production of tequila, filaments based on polylactic acid (PLA) were filled with agave fibers (0, 3, 5, 10 wt%), and further utilized to produce biocomposites by [...] Read more.
In order to provide a second economic life to agave fibers, an important waste material from the production of tequila, filaments based on polylactic acid (PLA) were filled with agave fibers (0, 3, 5, 10 wt%), and further utilized to produce biocomposites by fused deposition modeling (FDM)-based 3D printing at two raster angles (−45°/45° and 0°/90°). Differential scanning calorimetry, water uptake, density variation, morphology, and composting of the biocomposites were studied. The mechanical properties of the biocomposites (tensile, flexural, and Charpy impact properties) were determined following ASTM international norms. The addition of agave fibers to the filaments increased the crystallinity value from 23.7 to 44.1%. However, the fibers generated porous structures with a higher content of open cells and lower apparent densities than neat PLA pieces. The printing angle had a low significant effect on flexural and tensile properties, but directly affected the morphology of the printed biocomposites, positively influenced the impact strength, and slightly improved the absorption values for biocomposites printed at −45°/45°. Overall, increasing the concentrations of agave fibers had a detrimental effect on the mechanical properties of the biocomposites. The disintegration of the biocomposites under simulated composting conditions was slowed 1.6-fold with the addition of agave fibers, compared to neat PLA. Full article
(This article belongs to the Special Issue Functional and Architected Materials)
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<p>SEM micrographs of agave fibers (AF) used for biocomposite preparation (<b>A</b>) after sieving, and (<b>B</b>) after high shear mixing process (100× magnification).</p>
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<p>SEM micrographs of agave fibers/PLA biocomposites with different agave fiber content (0, 3, 5 and 10 wt%) and angle deposition (−45°/45° and 0°/90°) (70× magnification).</p>
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<p>Water absorption of agave fibers/PLA printed biocomposites at different agave fiber percentages (0, 3, 5, and 10 wt%) and (<b>A</b>) printing angle of −45°/45°, and (<b>B</b>) printing angle of 0°/90°.</p>
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<p>(<b>A</b>) Tensile strength and (<b>B</b>) tensile modulus of printed agave fibers/PLA biocomposites. The letters a–e on top of the bars indicates significant differences (<span class="html-italic">p</span> &lt; 0.05).</p>
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<p>(<b>A</b>) Flexural strength and (<b>B</b>) flexural modulus of printed agave fibers/PLA biocomposites. The letters a–f on top of the bars indicates significant differences (<span class="html-italic">p</span> &lt; 0.05).</p>
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<p>Charpy impact strength of printed agave fibers/PLA biocomposites. The letters a–b on top of the bars indicates significant differences (<span class="html-italic">p</span> &lt; 0.05).</p>
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<p>(<b>A</b>) Percentage weight losses of agave fiber/PLA printed biocomposites under simulated composting conditions and (<b>B</b>) photographs of agave fiber/PLA pieces after being composted.</p>
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