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Search Results (1,531)

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Keywords = fatigue experiment

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13 pages, 4567 KiB  
Article
Enhancing the Wear Resistance of CrAlN-Coated Tools in Milling and Turning Through Annealing with Optimized Duration
by Georgios Skordaris, Dimitrios Tsakalidis, Konstantinos-Dionysios Bouzakis, Fani Stergioudi and Antonios Bouzakis
Coatings 2025, 15(3), 311; https://doi.org/10.3390/coatings15030311 - 7 Mar 2025
Viewed by 71
Abstract
The work aimed to investigate the possibility of improving the mechanical properties, and therefore the wear resistance, of coated tools in manufacturing processes with continuous or interrupted cutting loads through appropriate annealing. In this context, PVD CrAlN coatings were deposited on cemented carbide [...] Read more.
The work aimed to investigate the possibility of improving the mechanical properties, and therefore the wear resistance, of coated tools in manufacturing processes with continuous or interrupted cutting loads through appropriate annealing. In this context, PVD CrAlN coatings were deposited on cemented carbide inserts. A part of these coated tools was annealed at a temperature of 400 °C, which was close to the deposition temperature, in an inert gas atmosphere. The annealing duration ranged up to 60 min. Nanoindentations and repeated perpendicular and inclined impact tests were carried out to characterize the strength, fatigue, and adhesion of the tool coatings before and after annealing. According to the results, the mechanical properties of the coating and the fatigue resistance were maximized after a short annealing period of about 15 min, while the adhesion of the coating remained unchanged. These facts led to a large increase in tool life in milling 42CrMo4 QT, when annealed coated tools were applied at 400 °C for 15 min. Furthermore, turning experiments using the mentioned hardened steel as well as GG30 cast iron to produce continuous or interrupted chips, respectively, confirmed the obtained results in milling. Therefore, annealing of coated cutting tools at an optimized duration is recommended as an effective method to extend tool life. Full article
(This article belongs to the Section Surface Characterization, Deposition and Modification)
24 pages, 17505 KiB  
Article
Bayesian Updating of Fatigue Crack Growth Parameters for Failure Prognosis of Miter Gates
by Anita Brown, Brian Eick, Travis Fillmore and Hai Nguyen
Materials 2025, 18(5), 1172; https://doi.org/10.3390/ma18051172 - 6 Mar 2025
Viewed by 143
Abstract
Navigable waterways play a vital role in the efficient transportation of millions of tons of cargo annually. Inland traffic must pass through a lock, which consists of miter gates. Failures and closures of these gates can significantly disrupt waterborne commerce. Miter gates often [...] Read more.
Navigable waterways play a vital role in the efficient transportation of millions of tons of cargo annually. Inland traffic must pass through a lock, which consists of miter gates. Failures and closures of these gates can significantly disrupt waterborne commerce. Miter gates often experience fatigue cracking due to their loading and welded connections. Repairing every crack can lead to excessive miter gate downtime and serious economic impacts. However, if the rate of crack growth is shown to be sufficiently slow, e.g., using Paris’ law, immediate repairs may be deemed unnecessary, and this downtime can be avoided. Paris’ law is often obtained from laboratory testing with detailed crack measurements of specimens with relatively simple geometry. However, Paris’ law parameters for an in situ structure will likely deviate from those predicted from physical testing due to variations in loading and materials and a far more complicated geometry. To improve Paris’ law parameter prediction, this research proposes a framework that utilizes (1) convenient vision-based tracking of crack evolution both in the laboratory and the field and (2) numerical model estimation of stress intensity factors (SIFs). This study’s methodology provides an efficient tool for Paris’ law parameter prediction that can be updated as more data become available through vision-based monitoring and provide actionable information about the criticality of existing cracks. Full article
(This article belongs to the Special Issue Evaluation of Fatigue and Creep-Fatigue Damage of Steel)
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<p>Methodology for determining crack growth parameters.</p>
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<p>Tracking crack progression by (<b>a</b>) determining crack initiation and location of the crack tip using strain field generated using DIC and (<b>b</b>) measuring the length of the crack over cycles.</p>
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<p>Selecting pixel coordinates to discretize the crack and determine total crack length.</p>
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<p>(<b>a</b>) Opening and closing of a miter gate and (<b>b</b>) application of hydrostatic load.</p>
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<p>Major components of a miter gate. Miter gate pictured is located at The Dalles Lock &amp; Dam (each leaf is approx. 32.4 m tall, 16.3 m wide).</p>
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<p>Cruciform specimen representative of the miter gate diaphragm and girder intersection and the full-scale physical test setup using a 220-kip actuator.</p>
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<p>Regions of specimen covered by camera setup. The fourth camera is monitoring the actuator.</p>
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<p>Numerical model of cruciform specimen.</p>
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<p>Partitioning and meshing scheme in region where crack initiates.</p>
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<p>(<b>a</b>,<b>b</b>) Location of crack initiation near CJP weld in pintle region circled in red; (<b>c</b>) difference in signed von Mises stress (ksi) between a gravity loading step and a combined gravity and hydrostatic loading step to indicate a significant change in stress.</p>
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<p>Location and approximate shape of crack on bottom girder.</p>
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<p>Inspection images: image with blue border (July 2023) contained the most points for comparison.</p>
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<p>Successfully transformed images overlayed.</p>
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<p>(<b>a</b>) Fully assembled miter gate leaf; (<b>b</b>) portion of bottom girder tied to pintle region. The solid portion of the girder is connected to the rest of the girder using shell-to-solid coupling.</p>
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<p>Numerical model boundary conditions.</p>
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<p>Crack propagation extracted using DIC plotted as crack length vs. number of cycles.</p>
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<p>Stress intensity factors extracted from numerical model plotted as K<sub>eq</sub> versus number of cycles.</p>
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<p>Crack growth rate versus SIF.</p>
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<p>Crack growth rate versus SIF and linear regression of all experimental data.</p>
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<p>Location of crack growth.</p>
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<p>(<b>a</b>) Predicted crack growth in ABAQUS using Paris’ law parameters estimated from standard linear regression; (<b>b</b>) example specimen from experimental crack growth for a maximum load of 489.3 kN (110 kips).</p>
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<p>New observations from inspection images with experimental data.</p>
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<p>Trace plots and posterior samples from MCMC simulations.</p>
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<p>Bayesian linear regression results.</p>
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<p>Predicted increment in crack growth (da) for number of cycles (dN) with varying SIF.</p>
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21 pages, 1386 KiB  
Article
Heart Rate Variability Biofeedback Training Can Improve Menopausal Symptoms and Psychological Well-Being in Women with a Diagnosis of Primary Breast Cancer: A Longitudinal Randomized Controlled Trial
by Karina Dolgilevica, Elizabeth Grunfeld and Nazanin Derakshan
Curr. Oncol. 2025, 32(3), 150; https://doi.org/10.3390/curroncol32030150 - 4 Mar 2025
Viewed by 269
Abstract
Breast cancer survivors experience numerous chronic symptoms linked to autonomic dysfunction including anxiety, stress, insomnia, menopausal symptoms, and cognitive impairment. Effective non-pharmacological solutions to address these are currently lacking. Methods: Our three-armed longitudinal randomized controlled trial assessed the effectiveness of a 4-week remote [...] Read more.
Breast cancer survivors experience numerous chronic symptoms linked to autonomic dysfunction including anxiety, stress, insomnia, menopausal symptoms, and cognitive impairment. Effective non-pharmacological solutions to address these are currently lacking. Methods: Our three-armed longitudinal randomized controlled trial assessed the effectiveness of a 4-week remote smartphone-based heart rate variability biofeedback intervention which involved daily paced breathing at 6 breaths p/min; active (12 breaths p/min) and waitlist controls were included. Heart rate variability and self-reported cancer-related symptoms were assessed at baseline, post-, and 6 months-post intervention. Participants were 60 UK-based women with primary breast cancer history (6 to 60 months post-active treatment). Results: The intervention group showed significant increases in low-frequency heart rate variability over time (F (4, 103.89) = 2.862, p = 0.027, d = 0.33), long-lasting improvement in sleep quality (F (4, 88.04) = 4.87, p = 0.001, d = 0.43) and cessations in night sweats (X2 (2, N = 59) = 6.44, p = 0.04, Cramer’s V = 0.33), and reduced anxiety post-intervention compared to the active and waitlist controls (F (4, 82.51) = 2.99, p = 0.023, d = 0.44). Other findings indicated that the intervention and active control participants reported lasting improvements in cognitive function, fatigue, and stress-related symptoms (all ps < 0.05). The waitlist group reported no symptom changes across time. Conclusion: Heart rate variability biofeedback is a feasible intervention for addressing diverse chronic symptoms commonly reported by breast cancer survivors. Full article
(This article belongs to the Special Issue Pathways to Recovery and Resilience in Breast Cancer Survivorship)
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<p>CONSORT diagram for heart rate variability biofeedback in breast cancer randomized controlled trial.</p>
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<p>Self-reported sleep quality at baseline, post-intervention, and at the 6 months follow-up; *** <span class="html-italic">p</span> &lt; 0.001, <span class="html-italic">ns p</span> &gt; 0.05.</p>
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<p>Number of cases reporting not having night sweats at baseline, post-intervention, and 6 months follow-up as compared to expected number of cases at each time-point.</p>
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23 pages, 2227 KiB  
Review
Evolution of the Fatigue Failure Prediction Process from Experiment to Artificial Intelligence: A Review
by Cornel Samoila, Doru Ursutiu and Iuliana Tudorache (Nistor)
Materials 2025, 18(5), 1153; https://doi.org/10.3390/ma18051153 - 4 Mar 2025
Viewed by 204
Abstract
An analysis of the time evolution of fatigue break prediction shows increasingly shorter developmental stages. The experimental period was the longest; the combination of more powerful mathematical methods led to a leap in evolution and a shortening of implementation time. All fatigue rupture [...] Read more.
An analysis of the time evolution of fatigue break prediction shows increasingly shorter developmental stages. The experimental period was the longest; the combination of more powerful mathematical methods led to a leap in evolution and a shortening of implementation time. All fatigue rupture prediction methods have proven to have limitations due to the multitude of influencing factors and the insufficient number of practical factors considered. Recently, attempts have been made to increase prediction accuracy by combining methods based on the physical mechanisms of the fatigue failure process with data-driven methods assisted by artificial intelligence. We attempt to present this evolution herein. There are several methods of review suitable for analyzing this subject: systematic, semi-systematic, and integrative. From these, a combination of semi-systematic and integrative was chosen precisely because the two methods complement each other. Full article
(This article belongs to the Section Mechanics of Materials)
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<p>Correlation between the amplitude stress intensity factor and crack growth.</p>
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<p>Schematic stress–life curve (Kohout–Vĕchet) [<a href="#B31-materials-18-01153" class="html-bibr">31</a>].</p>
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<p>Evolution of the approach to fatigue failure prediction.</p>
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<p>Basic components of AI, ML, and DL.</p>
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<p>Simulation model using ANN [<a href="#B72-materials-18-01153" class="html-bibr">72</a>].</p>
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<p>Layers in CNN networks.</p>
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<p>Structure of the CNN-LSTM model.</p>
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20 pages, 8314 KiB  
Article
Fatigue Enhancement Mechanism and Process Optimization of the Direct Mandrel Cold Expansion Technique on Lightweight and High-Strength Alloys
by Hansong Ji, Kanghua Huang, Li He, Zefeng Chen, Mingjun Tang, Pingfa Feng and Jianfu Zhang
J. Manuf. Mater. Process. 2025, 9(3), 81; https://doi.org/10.3390/jmmp9030081 - 3 Mar 2025
Viewed by 274
Abstract
Lightweight and high-strength alloys such as Al and Ti alloys are commonly employed materials for aviation structural components. A “hole-fastener” is commonly used for their connection, and DMCE (direct mandrel cold expansion) is a reliable technique in industries to enhance the fatigue properties [...] Read more.
Lightweight and high-strength alloys such as Al and Ti alloys are commonly employed materials for aviation structural components. A “hole-fastener” is commonly used for their connection, and DMCE (direct mandrel cold expansion) is a reliable technique in industries to enhance the fatigue properties of hole-involved components due to its advantages, i.e., convenient, efficient and cost-effective. However, an inadequate understanding of the DMCE process leads to a vast amount of waste in industries when any materials or structural parameters are changed. In order to promote the application efficiency of the DMCE process in aviation industries and reduce the energy and resource waste caused by repeated attempts, taking Al7050 and TB6 as examples, this paper comprehensively investigates the fatigue enhancement mechanism of the DMCE process on lightweight and high-strength alloys. Numerical models with 12.9%, 36.9% residual stress prediction errors and 9.98%, 14.8% radial plastic deformation prediction errors for Al and Ti holes were established, and then simulations were performed to screen out five significant influence parameters from eleven independent parameters. On this basis, DMCE experiments with significant parameters were carried out, and the improvement mechanisms of the DMCE process on the tangential residual stress, radial plastic deformation and surface morphology of Al and Ti hole walls were comparatively analyzed. Furthermore, fatigue life prediction models for two-hole-involved specimens were generated via multiple linear regression, which exhibit, respectively, 13.5% and 33.9% mean prediction errors for Al and Ti alloys. Moreover, the optimal DMCE schemes were obtained and 2.33 and 4.12 times fatigue lifetime improvements were achieved for the Al and the Ti specimens. Full article
24 pages, 4606 KiB  
Article
Finite Element Analysis of the Contact Pressure for Human–Seat Interaction with an Inserted Pneumatic Spring
by Xuan-Tien Tran, Van-Ha Nguyen and Duc-Toan Nguyen
Appl. Sci. 2025, 15(5), 2687; https://doi.org/10.3390/app15052687 - 3 Mar 2025
Viewed by 311
Abstract
This study explores the integration of a custom-designed pneumatic spring into a car-seat cushion and its interaction with a simplified human body model using the Finite Element Method (FEM). A 3D half-symmetry FEM framework, developed from experimental data, ensured computational efficiency and convergence. [...] Read more.
This study explores the integration of a custom-designed pneumatic spring into a car-seat cushion and its interaction with a simplified human body model using the Finite Element Method (FEM). A 3D half-symmetry FEM framework, developed from experimental data, ensured computational efficiency and convergence. This research bridged experimental and numerical approaches by analyzing the contact pressure distributions between a seat cushion and a volunteer with representative biometric characteristics. The model incorporated two material groups: (1) human body components (bones and muscles) and (2) seat cushion materials (polyurethane foam, latex, and fabric tape). Mechanical properties were obtained from both the literature and experiments, and simulations were conducted using MSC.Marc software under realistic boundary and initial conditions. The simulation results exhibited strong agreement with experimental data, validating the model’s reliability in predicting contact pressure distribution and optimizing seat cushion designs. Contrary to the conventional notion that uniformly distributed contact pressure inherently enhances comfort, this study emphasizes that the precise localization of pressure plays a crucial role in static and long-term seating ergonomics. Both experimental and simulation results demonstrated that modulating the pneumatic spring’s internal pressure from 0 kPa to 25 kPa altered peak contact pressure by approximately 3.5 kPa (around 20%), significantly influencing pressure redistribution and mitigating high-pressure zones. By validating this FEM-based approach, this study reduces dependence on physical prototyping, lowering design costs, and accelerating the development of ergonomically optimized seating solutions. The findings contribute to a deeper understanding of human–seat interactions, offering a foundation for next-generation automotive seating innovations that enhance comfort, fatigue reduction, and adaptive pressure control. Full article
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<p>A simplified scheme of the human–seat interaction.</p>
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<p>Structure and dimensions of the pneumatic spring [<a href="#B4-applsci-15-02687" class="html-bibr">4</a>].</p>
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<p>The electro-pneumatic control system.</p>
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<p>The skeletal component (<b>a</b>), soft tissue part (<b>b</b>), and biomechanical finite element (<b>c</b>) of the model. Colors were used to distinguish different types of component, including the sacrum (pink), pelvis (purple), femur (or-ange), the soft tissue layer (green), biomechanical finite element (Transparent color).</p>
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<p>Geometry and mesh of the right half-symmetric model of the car-seat cushion (<b>a</b>) and with the simplified pneumatic spring integrated inside (<b>b</b>). Colors were used to distinguish different component, including geometry (gray) and mesh (blue) of the right half-symmetric model, mesh of the rectangular block (green), mesh of the pneumatic spring integrated inside (yellow) (<b>c</b>).</p>
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<p>The compression test of polyurethane foam (<b>a</b>) and experimental results (<b>b</b>).</p>
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<p>Data for foam relaxation from the experiment.</p>
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<p>The experimental stress–strain curves (green square) and the fitted curves (solid green) from the foam compression test (<b>a</b>), along with the force–displacement diagram obtained from both the experiment and simulation (<b>b</b>).</p>
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<p>Circular membrane inflation test set up and the height of the hemisphere cap (<b>a</b>), displacement–pressure diagram of the test (<b>b</b>) and the strain–stress relationship (<b>c</b>).</p>
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<p>(<b>a</b>) Simulation results for the inflation test of a circular membrane, showing displacement in the z-direction [m]; (<b>b</b>) Simulation of the deformation behavior of the latex tube; (<b>c</b>) Comparison of experimental stress–strain data (blue) and fitted curves (red) for the latex membrane.</p>
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<p>(<b>a</b>) Uniaxial tensile testing setup for the fabric adhesive tape; (<b>b</b>) Experimental stress–strain curve (blue) compared with the fitted stress–strain curve (red) from the tensile test of the tape.</p>
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<p>The force distribution on the human body mode (<b>a</b>), contact table of the components in the model (<b>b</b>), the complete model (<b>c</b>), and the desired internal pressure of the pneumatic spring (<b>d</b>).</p>
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<p>The force distribution on the human body mode (<b>a</b>), contact table of the components in the model (<b>b</b>), the complete model (<b>c</b>), and the desired internal pressure of the pneumatic spring (<b>d</b>).</p>
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<p>The results of simulated (<b>a</b>) and experimental (<b>b</b>) contact pressure distribution.</p>
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<p>The desired internal pressure of the PSE from simulations (<b>left</b>) and experiments (<b>right</b>).</p>
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25 pages, 10008 KiB  
Article
Enhanced Erosion Resistance of Cr3C2-TiC-NiCrCoMo Coatings: Experimental and Numerical Investigation of Erosion Mechanisms
by Jiawei Wang, Linwen Wang, Haiyang Lu, Jiyu Du, Xiaoxia Qi, Laixiao Lu, Yanhua Zhao, Ziwu Liu and Weiyun Meng
Coatings 2025, 15(3), 294; https://doi.org/10.3390/coatings15030294 - 3 Mar 2025
Viewed by 271
Abstract
To enhance the erosion resistance of typical Cr3C2-NiCr coatings, the Cr3C2-TiC-NiCrCoMo (NCT) coating was developed and deposited by high-velocity oxygen fuel spray (HVOF). The erosion resistance and mechanisms of the coating were investigated using numerical [...] Read more.
To enhance the erosion resistance of typical Cr3C2-NiCr coatings, the Cr3C2-TiC-NiCrCoMo (NCT) coating was developed and deposited by high-velocity oxygen fuel spray (HVOF). The erosion resistance and mechanisms of the coating were investigated using numerical simulations and experimental methods. A comprehensive calculation model for the coating erosion rate was developed, incorporating factors such as the properties of the eroded particles, the characteristics of the coating, and the conditions of erosion. The erosion rate of the NCT coating was calculated and predicted by the model, and the accuracy of these predictions was validated through experiments. The NCT1 (87.3 wt.% Cr3C2-NiCrCoMo/3 wt.% TiC)coating demonstrated exceptional erosion resistance compared to the original Cr3C2-NiCrCoMo (NCC) coatings with reduced erosion rates of 23.64%, 20.45%, and 16.22% at impact angles of 30°, 60°, and 90°, respectively. The addition of nano-TiC particles into the NCT1 coating enhances the yield strength, impeding the intrusion of erosive particles at low angles and supporting the metal binder phase, eventually reducing fatigue fracture under repeated erosion. However, excessive nano-TiC content degrades the erosion resistance due to the increase in pores and cracks within the coating. Full article
(This article belongs to the Special Issue Laser Technology of Thin Film and Coatings)
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<p>Structure diagram of high-speed airflow sandblasting erosion wear tester.</p>
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<p>High-speed airflow sandblasting erosion wear tester.</p>
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<p>Typical load–displacement curve.</p>
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<p>Schematic diagram of particle impact in normal direction.</p>
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<p>Schematic diagram of contact stress between particle and coating.</p>
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<p>Comparison between actual and simulated erosion rate of Cr<sub>3</sub>C<sub>2</sub>-NiCr coating.</p>
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<p>Microstructure of NCC and NCT coating, (<b>a</b>) NCC, (<b>b</b>) NCT1, (<b>c</b>) NCT2.</p>
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<p>XRD pattern of NCC and NCT coating.</p>
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<p>Microhardness of NCC and NCT coating.</p>
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<p>Tensile bonding strength of NCC and NCT coating.</p>
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<p>Erosion rates of the coating at different impact angles at normal temperature.</p>
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<p>Surface erosion profile on the coating surface at different impact angles at normal temperature, (<b>a</b>) NCC-30°, (<b>b</b>) NCT1-30°, (<b>c</b>) NCT2-30°, (<b>d</b>) NCC-60°, (<b>e</b>) NCT1-60°, (<b>f</b>) NCT2-60°, (<b>g</b>) NCC-90°, (<b>h</b>) NCT1-90°, (<b>i</b>) NCT2-90°.</p>
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<p>Microstructure of the erosion area on the coating surface at norma, (<b>a</b>) NCC-30°, (<b>b</b>) NCT1-30°, (<b>c</b>) NCT2-30°, (<b>d</b>) NCC-60°, (<b>e</b>) NCT1-60°, (<b>f</b>) NCT2-60°, (<b>g</b>) NCC-90°, (<b>h</b>) NCT1-90°, (<b>i</b>) NCT2-90°.</p>
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<p>Microstructure of the NCC and NCT2 coatings at a 90° impact angle, (<b>a</b>) NCC-30°, (<b>b</b>) NCT1-30°, (<b>c</b>) NCT2-30°, (<b>d</b>) NCC-60°, (<b>e</b>) NCT1-60°, (<b>f</b>) NCT2-60°, (<b>g</b>) NCC-90°, (<b>h</b>) NCT1-90°, (<b>i</b>) NCT2-90°.</p>
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<p>Schematic diagram of coating erosion at normal temperature.</p>
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18 pages, 12649 KiB  
Article
A Microplane Model That Considers Dynamic Fatigue Damage and Its Applications in Concrete Infrastructure
by Changjin Qin, Xiaogang Dong, Biao Wu, Lidong Cai, Shaohua Wang and Qing Xia
Infrastructures 2025, 10(3), 49; https://doi.org/10.3390/infrastructures10030049 - 28 Feb 2025
Viewed by 135
Abstract
In significant infrastructure, it takes more than simple fatigue load capacity calibration to meet design and analysis requirements; more importantly, fatigue damage evolution and remaining life assessments should be undertaken. Therefore, this paper proposes a dynamic fatigue damage analysis method for concrete infrastructures [...] Read more.
In significant infrastructure, it takes more than simple fatigue load capacity calibration to meet design and analysis requirements; more importantly, fatigue damage evolution and remaining life assessments should be undertaken. Therefore, this paper proposes a dynamic fatigue damage analysis method for concrete infrastructures based on an extended microplane model. This study extends the original microplane model to encompass steel fiber-reinforced concrete, fatigue, and dynamic analysis. In particular, the influence of the material rate-dependent effect (usually related to loading frequency) on the material’s properties is considered. The model’s validity is corroborated through benchmark tests and illustrative examples. Subsequently, the model is employed for the dynamic fatigue analysis of concrete members and concrete infrastructure, with a particular focus on the material rate-dependent effects and the influence of steel fiber on the fatigue behavior of concrete. It is demonstrated that incorporating steel fiber into concrete can markedly enhance its fatigue resistance, a phenomenon that can be reflected in the present model. Furthermore, accelerated fatigue experiments may overestimate the fatigue life of concrete materials. However, when conducting dynamic fatigue analysis of structures, incorporating rate-dependent materials may result in underestimating the fatigue damage experienced by concrete infrastructures. The model provides a helpful predictive tool for assessing progressive fatigue damage in concrete infrastructure under a complex range of loading scenarios, contributing to structural resilience and promoting sustainability. Full article
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<p>Stress–strain boundaries on the microplane.</p>
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<p>Comparison of simulated and experimental experiments for side-limited uniaxial compression.</p>
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<p>Changes in energy during calculations of microplane model.</p>
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<p>The setup of the three-point bending beam experimental for concrete.</p>
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<p>Load–displacement curve at loading point.</p>
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<p>Geometry, boundary conditions, and loading of reinforced concrete beams.</p>
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<p>Cracking pattern of RC beam (<math display="inline"><semantics> <mrow> <mi>D</mi> <mo>=</mo> <mn>400</mn> <mo> </mo> <mi mathvariant="normal">m</mi> <mi mathvariant="normal">m</mi> </mrow> </semantics></math>) in shear for loads <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>P</mi> </mrow> <mrow> <mi mathvariant="normal">m</mi> <mi mathvariant="normal">a</mi> <mi mathvariant="normal">x</mi> </mrow> </msub> <mo>/</mo> <mn>3</mn> </mrow> </semantics></math> and <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>P</mi> </mrow> <mrow> <mi mathvariant="normal">m</mi> <mi mathvariant="normal">a</mi> <mi mathvariant="normal">x</mi> </mrow> </msub> </mrow> </semantics></math>.</p>
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<p>Cracking pattern of RC beam (<math display="inline"><semantics> <mrow> <mi>D</mi> <mo>=</mo> <mn>800</mn> <mo> </mo> <mi mathvariant="normal">m</mi> <mi mathvariant="normal">m</mi> </mrow> </semantics></math>) in shear for loads <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>P</mi> </mrow> <mrow> <mi mathvariant="normal">m</mi> <mi mathvariant="normal">a</mi> <mi mathvariant="normal">x</mi> </mrow> </msub> <mo>/</mo> <mn>3</mn> </mrow> </semantics></math> and <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>P</mi> </mrow> <mrow> <mi mathvariant="normal">m</mi> <mi mathvariant="normal">a</mi> <mi mathvariant="normal">x</mi> </mrow> </msub> </mrow> </semantics></math>.</p>
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<p>Stress–strain curves measured at different strain rates fitted to microplane model.</p>
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<p>Consideration of material strain rate effects on fatigue life.</p>
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<p>Consideration of material strain rate effects on fatigue life.</p>
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<p>Geometry of the test bench foundation.</p>
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<p>Load and boundary condition of the test bench foundation.</p>
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<p>Finite element mesh of the test bench foundation.</p>
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<p>Stresses and strains in the concrete foundation under static load (plain concrete).</p>
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<p>Stresses and strains in the concrete foundation under static load (SFRC).</p>
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<p>Stresses and strains in the concrete foundation under fatigue load (plain concrete, 100th load, without rate-dependent effects).</p>
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<p>Stresses and strains in the concrete foundation under fatigue load (steel fiber-reinforced concrete, 100th load, without rate-dependent effects).</p>
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<p>Stresses and strains in the concrete foundation under fatigue load (plain concrete, reinforced concrete, 100th load, with rate-dependent effects).</p>
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<p>Stresses and strains in the concrete foundation under fatigue load (steel fiber-reinforced concrete, 100th load, with rate-dependent effects).</p>
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19 pages, 1962 KiB  
Article
A Novel Bilinear Traction-Separation Law for Fatigue Damage Accumulation of Adhesive Joints in Fiber-Reinforced Composite Material Under Step/Variable-Amplitude Loading
by Abinash Patro and Ala Tabiei
J. Compos. Sci. 2025, 9(3), 112; https://doi.org/10.3390/jcs9030112 - 27 Feb 2025
Viewed by 107
Abstract
Adhesive joints in real-world conditions often experience variable or step loading rather than constant-amplitude fatigue. This study addresses this gap by examining the influence of load sequence and block loading on fatigue damage in adhesive joints of fiber-reinforced polymer (FRP) composites. A novel [...] Read more.
Adhesive joints in real-world conditions often experience variable or step loading rather than constant-amplitude fatigue. This study addresses this gap by examining the influence of load sequence and block loading on fatigue damage in adhesive joints of fiber-reinforced polymer (FRP) composites. A novel bilinear traction-separation law based on the Fatigue Crack Growth Rate (FCGR) rule is introduced to predict fatigue failure under step/variable loads, accounting for load history, sequence, and interaction effects. This model was validated using a double-lap joint model under step/variable loading across four experimental scenarios. The proposed model outperformed existing fatigue damage-accumulation models, significantly reducing the Relative Error of Prediction (REP). Notably, the proposed model significantly reduced the Relative Error of Prediction (REP), achieving reductions from 81.10% to as low as 0.013% in certain cases. The proposed bilinear law exhibited an accelerated damage accumulation rate per cycle for low-to-high loading situations and a decelerated rate for high-to-low loading scenarios, aligning more closely with experimental observations. The proposed model offers practical benefits by improving fatigue life predictions, enabling optimized FRP composite designs, and minimizing overengineering. These advancements are particularly relevant in industries such as aerospace, automotive, and wind energy, where structural durability and safety are paramount. This research represents a significant step forward in the fatigue analysis of composite adhesive joints, paving the way for more reliable engineering solutions. Full article
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<p>Theoretical High-to-Low and Low-to-High Loading sequences and hypothetical damage-accumulation illustration. The total damage is denoted by <span class="html-italic">D</span>, <math display="inline"><semantics> <msub> <mi>n</mi> <mi>i</mi> </msub> </semantics></math> represents the number of fatigue cycles at the <span class="html-italic">i</span>th constant-amplitude loading stage, and <math display="inline"><semantics> <msub> <mi>N</mi> <mi>i</mi> </msub> </semantics></math> signifies the number of fatigue cycles until failure occurs at the <span class="html-italic">i</span>th constant-amplitude loading stage.</p>
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<p>Typical cohesive zone model and its Bilinear Traction-Separation (S–N) Law.</p>
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<p>Energy release rate under Paris Law.</p>
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<p>Example of Step Loading used in the simulation.</p>
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<p>Specification of double-lap joint used in the study.</p>
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<p>Comparison of Experimental Data and Simulation for constant load fatigue test [<a href="#B12-jcs-09-00112" class="html-bibr">12</a>].</p>
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<p>Comparison of fatigue failure of step-loading cases between experimental data, original bilinear traction separation law, and proposed bilinear traction separation law [<a href="#B12-jcs-09-00112" class="html-bibr">12</a>]. Low-to-high load transition Cases (<b>Case 1</b>) 14400 N to 21600 N and (<b>Case 2</b>) 12000 N to 19200 N. High-to-Low Load transition Cases (<b>Case 3</b>) 21600 N to 14400 N and (<b>Case 4</b>) 19200 N to 12000 N.</p>
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<p>Comparison of damage-accumulation rate per cycle after load transition or load level 2 between the original bilinear traction-separation law and the proposed traction-separation law. Examples (<b>a</b>) Low-to-high loading Case 2 and (<b>b</b>) High-to-Low loading Case 4.</p>
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<p>Comparison of percentage error deviation of number of cycles to failure between experimental data, proposed bilinear traction-separation law, original bilinear traction-separation law, and other theoretical models. Low-to-high load transition cases (Case 1) 14400 N to 21600 N and (Case 4) High-to-low load transition cases 19200 N to 12000 N.</p>
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18 pages, 12155 KiB  
Article
The Fatigue Behavior of TC4 and Ti60 Dissimilar Titanium Alloy Joints Welded by Electron Beam
by Shiqing Wang, Xiangyong Zhu, Wenyan Zhai, Qian Gao and Yongxin Lu
Crystals 2025, 15(3), 224; https://doi.org/10.3390/cryst15030224 - 26 Feb 2025
Viewed by 219
Abstract
During use, titanium alloy structural components may experience sudden overloads or occasional loads, which can reduce their fatigue life and accelerate structural failure. To study the fatigue behavior of TC4/Ti60 joints, this paper uses electron beam welding technology to obtain TC4/Ti60 dissimilar joints. [...] Read more.
During use, titanium alloy structural components may experience sudden overloads or occasional loads, which can reduce their fatigue life and accelerate structural failure. To study the fatigue behavior of TC4/Ti60 joints, this paper uses electron beam welding technology to obtain TC4/Ti60 dissimilar joints. The results show that the microstructure changes during the welding process, with the weld zone being relatively uniform, primarily consisting of coarse α′ phase. The near heat-affected zone on the TC4 side consists of α′, while on the Ti60 side, in addition to the α′ phase, there is a small amount of residual α phase. Fatigue tests reveal that as the pre-deformation increases, the fatigue life gradually decreases. During the early stages of fatigue, the joint exhibits cyclic hardening, which transitions to cyclic softening as the test progresses, ultimately leading to failure. Fatigue fracture analysis reveals that all fatigue samples failed on the TC4 side, with no failure observed in the weld zone. This is likely due to the presence of martensite, which gives the weld zone higher strength than the TC4 base materials. Additionally, fatigue cracks initiated from surface or near-surface defects, with ductile fractures being predominant. Full article
(This article belongs to the Special Issue Development of Light Alloys and Their Applications)
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<p>Specimen configurations of TC4/Ti60 for tensile test (mm).</p>
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<p>Specimen configurations of TC4/Ti60 for fatigue test (mm).</p>
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<p>Microstructural characterization obtained by OM and EBSD. (<b>a</b>,<b>b</b>) TC4 titanium alloy, (<b>c</b>,<b>d</b>) Ti60 titanium alloy.</p>
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<p>Microstructure of the joint between TC4 and Ti60 alloys. (<b>a</b>) TC4 far-HAZ, (<b>b</b>) TC4 near HAZ, (<b>c</b>) fusion line between WZ and TC4 HAZ, (<b>d</b>) WZ, (<b>e</b>) Ti60 near HAZ, (<b>f</b>) Ti60 far-HAZ.</p>
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<p>Tensile test results of the specimens.</p>
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<p>Typical stress–strain hysteresis loops of TC4/Ti60 joint. (<b>a</b>) The first cycle under different pre-deformations: (<b>b</b>) 0 mm cyclic hysteresis loop, (<b>c</b>) 0.5 mm cyclic hysteresis loop, (<b>d</b>) 1 mm cyclic hysteresis loop, (<b>e</b>) 1.5 mm cyclic hysteresis loop.</p>
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<p>Typical stress–strain hysteresis loops of TC4/Ti60 joint. (<b>a</b>) The first cycle under different pre-deformations: (<b>b</b>) 0 mm cyclic hysteresis loop, (<b>c</b>) 0.5 mm cyclic hysteresis loop, (<b>d</b>) 1 mm cyclic hysteresis loop, (<b>e</b>) 1.5 mm cyclic hysteresis loop.</p>
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<p>Typical stress–strain hysteresis loops of TC4/Ti60 joint. (<b>a</b>) The first cycle under different pre-deformations: (<b>b</b>) 0 mm cyclic hysteresis loop, (<b>c</b>) 0.5 mm cyclic hysteresis loop, (<b>d</b>) 1 mm cyclic hysteresis loop, (<b>e</b>) 1.5 mm cyclic hysteresis loop.</p>
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<p>Stress amplitude vs. the number of cycles at different pre-deformation.</p>
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<p>Plastic strain amplitude vs. the number of cycles at different pre-deformation levels.</p>
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<p>Modulus vs. the number of cycles at different pre-deformation levels. (<b>a</b>) Loading modulus, (<b>b</b>) unloading modulus.</p>
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<p>Modulus vs. the number of cycles at different pre-deformation levels. (<b>a</b>) Loading modulus, (<b>b</b>) unloading modulus.</p>
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<p>The number of cyclic to failure of the dissimilar joints under different pre-deformation levels.</p>
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<p>The pore defect.</p>
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<p>Surface morphologies of the tensile fracture surfaces of dissimilar joints under different magnifications at the TC4 side. (<b>a</b>,<b>b</b>) Fracture morphology under low magnification, (<b>c</b>,<b>d</b>) fracture morphology under high magnification.</p>
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<p>An overall view of fracture surfaces of the fatigued joint on the TC4 side under pre-deformations of (<b>a</b>) 0.5 mm and (<b>b</b>) 1.5 mm.</p>
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<p>SEM images of fracture surfaces for the fatigued joint on the TC4 side at pre-deformations of (<b>a</b>,<b>c</b>,<b>e</b>) 0.5 mm, and (<b>b</b>,<b>d</b>,<b>f</b>) 1.5 mm. (<b>a</b>,<b>b</b>) Fatigue-crack-initiation region, (<b>c</b>,<b>d</b>) propagation region, (<b>e</b>,<b>f</b>) fast-fracture region.</p>
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<p>SEM images of fracture surfaces for the fatigued joint on the TC4 side at pre-deformations of (<b>a</b>,<b>c</b>,<b>e</b>) 0.5 mm, and (<b>b</b>,<b>d</b>,<b>f</b>) 1.5 mm. (<b>a</b>,<b>b</b>) Fatigue-crack-initiation region, (<b>c</b>,<b>d</b>) propagation region, (<b>e</b>,<b>f</b>) fast-fracture region.</p>
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13 pages, 230 KiB  
Article
Feasibility and Acceptability of Social Prescribing for Cancer Survivors
by Deirdre Connolly, Chloe O’Hara, Catherine O’Brien and Adrienne Dempsey
Curr. Oncol. 2025, 32(3), 129; https://doi.org/10.3390/curroncol32030129 - 25 Feb 2025
Viewed by 183
Abstract
Following cancer treatment, individuals experience a range of physical, mental and social health difficulties that interfere with their ability to resume participation in pre-cancer activities. In Ireland, the National Cancer Strategy recommends community-based services to address post-treatment difficulties. Social prescribing is a community-based, [...] Read more.
Following cancer treatment, individuals experience a range of physical, mental and social health difficulties that interfere with their ability to resume participation in pre-cancer activities. In Ireland, the National Cancer Strategy recommends community-based services to address post-treatment difficulties. Social prescribing is a community-based, non-medical service that links individuals with health-related activities and supports in their community. This study explored the feasibility and acceptability of social prescribing for cancer survivors. A mixed methods study was undertaken with individuals who had completed curative treatment for any cancer type. Recruitment was carried out in a national cancer centre. Quantitative outcomes included feasibility metrics (recruitment, intervention adherence and retention), the Frenchay Activities Index (FAI), the Hospital Depression and Anxiety Scale (HADS), the Multidimensional Assessment of Fatigue (MAF), and EORTC QLQ-C30. Qualitative interviews explored acceptability of social prescribing. Data were analysed using descriptive statistics (quantitative data) and content analysis (qualitative data). Out of 131 individuals identified as eligible to participate, 43 agreed to participate (32.8% recruitment) and 27 met a link worker and were connected to a local activity (62.7% adherence) and completed follow-up outcome measures (62.7% retention). Improvements were observed in all health-related outcomes and those interviewed identified the intervention as acceptable. Study participants attended a range of community-based activities as a result of link worker support. They also reported increased confidence, improved mental health and reduction in fatigue following attendance at community-based activities. The findings of this study indicate that social prescribing is a feasible and acceptable community-based intervention to improve the physical, mental and social health of individuals living with and beyond cancer. A pilot randomised trial is indicated to inform a definitive intervention trial. Full article
(This article belongs to the Section Psychosocial Oncology)
21 pages, 2644 KiB  
Review
Comparative Analysis of Wear Models for Accurate Wear Predictions
by Guntis Springis and Irina Boiko
Lubricants 2025, 13(3), 100; https://doi.org/10.3390/lubricants13030100 - 25 Feb 2025
Viewed by 307
Abstract
The development of innovative technologies and the employment of diverse material compositions have contributed to the enhancement of wear prediction methods. However, the accurate forecasting of service life and the identification of critical influencing factors remain challenging due to the complex interactions governing [...] Read more.
The development of innovative technologies and the employment of diverse material compositions have contributed to the enhancement of wear prediction methods. However, the accurate forecasting of service life and the identification of critical influencing factors remain challenging due to the complex interactions governing wear behaviour. Throughout history, various methodological approaches have been developed to model wear, primarily categorised into analytical calculations and experimental investigations. Analytical methods, including Archard’s equation and its variations, provide a theoretical basis for wear estimation. However, these models frequently depend on empirical coefficients derived from extensive experimentation, which restricts their predictive accuracy. Moreover, classical wear models do not fully account for material fatigue effects and 3D surface texture parameters, which are critical for solving complex engineering problems. Recent advancements have sought to address these limitations by integrating probabilistic surface modelling, fatigue-based degradation theories, and numerical simulations to enhance wear predictions. Experimental investigations remain essential for validating analytical models, as they provide empirical data necessary for parameter calibration. However, these experiments require specialised equipment and are often time-consuming and costly. The integration of modern measurement tools and numerical simulations, such as finite element analysis (FEA) and machine learning-based models, presents a promising direction for improving wear predictions. This review highlights the strengths and limitations of existing wear models and emphasises the need for further refinement of analytical approaches to incorporate fatigue wear mechanisms, real surface roughness effects, and environmental influences for more accurate and reliable wear assessments. Full article
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<p>Process of wear simulation based on Archard’s wear law [<a href="#B7-lubricants-13-00100" class="html-bibr">7</a>].</p>
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<p>Shape of the active components (<b>left</b>: lower blade; <b>right</b>: upper blade) before and after 100,000 cutting cycles [<a href="#B8-lubricants-13-00100" class="html-bibr">8</a>].</p>
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<p>Experimental and simulative worn profiles of the lower and upper blades after 100,000 strokes [<a href="#B8-lubricants-13-00100" class="html-bibr">8</a>].</p>
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<p>A wear track with characteristic c-cracks on the surface after a 30 min test (<b>left</b>), along with a cross-sectional view of wear tracks (waviness profiles) over time (<b>right</b>) [<a href="#B14-lubricants-13-00100" class="html-bibr">14</a>].</p>
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<p>Flow diagram for analysing wear and mechanical behaviour of intersecting steel wires.</p>
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<p>Bottom and side views of wear using both the MC-SPG method (<b>a</b>) and the wear model (<b>b</b>) [<a href="#B19-lubricants-13-00100" class="html-bibr">19</a>].</p>
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21 pages, 20371 KiB  
Article
Comparison of Three Methods of Measuring Residual Stresses in Welded Joints of High-Strength Steel S960QL
by Mirza Manjgo, Gorazd Lojen, Nenad Gubeljak, Blaž Karpe and Tomaž Vuherer
Materials 2025, 18(5), 950; https://doi.org/10.3390/ma18050950 - 21 Feb 2025
Viewed by 251
Abstract
The influence of residual stresses as a result of the welding process in the overall stress state of the weld joint is of great importance because they significantly affect the creation and growth of cracks, the occurrence of brittle fracture, and material fatigue. [...] Read more.
The influence of residual stresses as a result of the welding process in the overall stress state of the weld joint is of great importance because they significantly affect the creation and growth of cracks, the occurrence of brittle fracture, and material fatigue. Previous experiences indicate that it would be necessary to provide an assessment of the deformation and stress state in the critical zones of the weld joints using a suitable test method, which will not endanger the structural integrity of the tested places. There are different methods for measurement of residual stress in welded constructions: destructive, semi-destructive and non-destructive. To choose one method over another, it is necessary to take into account the advantages and limitations of these techniques for practical application. This paper considers and analyzes the residual stresses in the welded joint of high-strength steel S960QL. MAG welding was performed by a robot. Three methods were used to measure the residual stresses: the magnetic method (MAS), the X-ray diffraction method (XRD), and the hole drilling method (HD). By all three methods, the highest residual stresses were measured in the weld metal and in the heat-affected zones. Nevertheless, the measured values differed considerably. The differences can be contributed to (a) the kind of stress that the individual method measures, (b) to the volume of material from which each method captures the signal and averages it, and (c) to the different sensitivities of the applied methods to coarse-grained microstructure and microstructural gradients. Full article
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<p>Longitudinal residual stresses in welded austenitic stainless steel, where no phase transformations in the solid state occur; red: tensile stress, blue: compressive stress.</p>
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<p>Welded construction steel, subjected to phase transformations in the solid state. Total residual stress distribution along several crystal grains of a polycrystalline material and their partitioning in type I (<span class="html-italic">σ</span><sup>RS,I</sup>.—macro residual stresses), type II (<span class="html-italic">σ</span><sup>RS,II</sup>.—homogeneous micro residual stresses) and type III and type IV (<span class="html-italic">σ</span><sup>RS,III</sup>.—inhomogeneous micro residual stresses inside grains and <span class="html-italic">σ</span><sup>RS,IV</sup>.—inhomogeneous micro residual stresses between grains and grain boundary).</p>
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<p>(<b>a</b>) Geometry of the weld groove; (<b>b</b>) sequence of weld passes.</p>
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<p>Geometry of tensile specimens.</p>
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<p>Coordinates of measuring points (see <a href="#materials-18-00950-t005" class="html-table">Table 5</a>).</p>
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<p>(<b>a</b>) SMMT-1 was used for measurement; (<b>b</b>) a tensile test specimen was used for calibration.</p>
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<p>Calibration curve of stress–signal voltage.</p>
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<p>Measuring device PULSTEC U-X360 for the XRD method.</p>
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<p>The device MTS3000 RESTAN for centering the drill and drilling a hole at residual stress measurement.</p>
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<p>Microstructures in three areas of the weld join.</p>
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<p>Subtraction of the principal residual stresses <span class="html-italic">σ</span><sub>1</sub>–<span class="html-italic">σ</span><sub>2</sub>, measured by the magnetic method.</p>
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<p>Residual stresses in the longitudinal and transverse directions measured by the X-ray diffraction method.</p>
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<p>The Subtraction of longitudinal and transverse residual stresses <span class="html-italic">σ</span><sub>long</sub>–<span class="html-italic">σ</span><sub>tran</sub> measured by X-ray diffraction.</p>
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<p>Measured residual stresses by the hole drilling method for measuring point M1—base material: (<b>a</b>) measured deformations in individual strain gauges; (<b>b</b>) measured principal stresses and angles; (<b>c</b>) measured longitudinal, transverse and shear stresses.</p>
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<p>Measured residual stresses by the hole drilling method for measuring point M4—heat-affected zone: (<b>a</b>) measured deformations in individual strain gauges; (<b>b</b>) measured principal stresses and angles; (<b>c</b>) measured longitudinal, transverse and shear stresses.</p>
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<p>Measured residual stresses by the hole drilling method for measuring point M5—weld metal: (<b>a</b>) measured deformations in individual strain gauges; (<b>b</b>) measured principal stresses and angles; (<b>c</b>) measured longitudinal, transverse and shear stresses.</p>
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<p>Subtraction of longitudinal and transverse residual stresses <span class="html-italic">σ</span><sub>long</sub>–<span class="html-italic">σ</span><sub>tran</sub> measured by the hole drilling method at a depth of 1 mm.</p>
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<p>Microstructure: (<b>a</b>) base material; (<b>b</b>) HAZ; (<b>c</b>) WM—weld metal at weld toe.</p>
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<p>Comparison of longitudinal residual stresses between the HD and XRD methods.</p>
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<p>Comparison of transverse residual stresses between the HD and XRD methods.</p>
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<p>Comparison of the subtractions of longitudinal and transverse residual stresses <span class="html-italic">σ</span><sub>long</sub> −<span class="html-italic">σ</span><sub>tran</sub> between all three measurement methods.</p>
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18 pages, 6377 KiB  
Article
The Effect of the Corrosion Degree of Prestressed Steel Reinforcements on the Strain of Concrete Box Girders: An Experimental Fatigue Study
by Zhao-Yuan Zhang, Ping Wei, Peng Cao and Hai-Bin Huang
Buildings 2025, 15(5), 655; https://doi.org/10.3390/buildings15050655 - 20 Feb 2025
Viewed by 189
Abstract
In order to investigate the relationship between the strain of prestressed concrete girders under fatigue loading and the corrosion degree of prestressed steel reinforcements, four 12.4-m-long large-size post-tensioned prestressed concrete box girders were designed and fabricated in this study, and prestressed steel reinforcements [...] Read more.
In order to investigate the relationship between the strain of prestressed concrete girders under fatigue loading and the corrosion degree of prestressed steel reinforcements, four 12.4-m-long large-size post-tensioned prestressed concrete box girders were designed and fabricated in this study, and prestressed steel reinforcements were corroded at different degrees by the Electric Accelerated Corrosion Method. The same equal-amplitude loads were used during fatigue loading. The relationship between the strain of different materials (strains of the plain reinforcements and prestressed steel reinforcements, as well as concrete strains in compression zones) and the corrosion degree was investigated. Then, the calculation method for the cumulative residual strain of concrete in the compression zone of the test beam was obtained. The test results show the following: the strains of the test beams under different corrosion degrees all show a three-stage development law; the ratio of the strain amplitude of the prestressed steel reinforcement to that of the regular steel reinforcement during fatigue loading basically stays in the range of 0.65–0.75, and the ratio rises with the corrosion degree of the prestressed steel reinforcement; the increase in strain of the compressed concrete is due to the accumulation of the residual strain of the concrete, and the increase in material strain is almost directly proportional to the growth of corrosion degree under the same fatigue load; the calculated values of the accumulated residual strain of the concrete agree well with the test values and satisfy the accuracy requirements of engineering. Full article
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<p>Arrangement of prestressed reinforcement in the test beam (cm). (<b>a</b>) Half elevation of vertical arrangement of longitudinal prestressed reinforcement in the test girder. (<b>b</b>) Distribution of prestressed reinforcement in the section of the pivot point. (<b>c</b>) Distribution of prestressed reinforcement in mid-span section.</p>
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<p>Arrangement of ordinary reinforcement in the test beam (cm). (<b>a</b>) Half elevation of ordinary reinforcement in test beam. (<b>b</b>) Distribution of ordinary reinforcement in the pivot section. (<b>c</b>) Distribution of ordinary reinforcement in mid-span section.</p>
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<p>Structural drawing of corrosion tank.</p>
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<p>CAD schematic diagram of the loading experiment (cm).</p>
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<p>Test beam load–deflection curve at mid-span.</p>
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<p>Schematic diagram of test beam S1’s elevation cracks.</p>
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<p>Fracture surface of corroded prestressed strand wire in this test.</p>
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<p>All fracture surfaces and fracture modes of the strand wires at the breakage location.</p>
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<p>Crack distribution in the final stage of fatigue loading of test beams. (<b>a</b>) F-0. (<b>b</b>) F-4. (<b>c</b>) F-8.</p>
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<p>Strain changes in ordinary steel reinforcements under fatigue loading. (<b>a</b>) F-0: load–ordinary reinforcement strain curve. (<b>b</b>) F-0: variation in strain with number of fatigue loadings in ordinary steel reinforcement. (<b>c</b>) F-4: load–ordinary reinforcement strain curve. (<b>d</b>) F-4: variation in strain with number of fatigue loadings in ordinary steel reinforcement. (<b>e</b>) F-8: load–ordinary reinforcement strain curve. (<b>f</b>) F-8: variation in strain with number of fatigue loadings in ordinary steel reinforcement.</p>
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<p>Strain changes in ordinary steel reinforcements under fatigue loading. (<b>a</b>) F-0: load–ordinary reinforcement strain curve. (<b>b</b>) F-0: variation in strain with number of fatigue loadings in ordinary steel reinforcement. (<b>c</b>) F-4: load–ordinary reinforcement strain curve. (<b>d</b>) F-4: variation in strain with number of fatigue loadings in ordinary steel reinforcement. (<b>e</b>) F-8: load–ordinary reinforcement strain curve. (<b>f</b>) F-8: variation in strain with number of fatigue loadings in ordinary steel reinforcement.</p>
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<p>Strain variation in prestressed reinforcements under fatigue loading. (<b>a</b>) F-0: load–prestressed reinforcement strain curve. (<b>b</b>) F-0: relationship between strain and number of fatigue loadings of prestressed reinforcement. (<b>c</b>) F-4: load–prestressed reinforcement strain curve. (<b>d</b>) F-4: relationship between strain and number of fatigue loadings of prestressed reinforcement. (<b>e</b>) F-8: load–prestressed reinforcement strain curve. (<b>f</b>) F-8: relationship between strain and number of fatigue loadings of prestressed reinforcement.</p>
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<p>The ratio between the strain amplitude of prestressed reinforcements and ordinary reinforcements under fatigue loading.</p>
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<p>Concrete strain changes in the compression zone of test beams during fatigue loading. (<b>a</b>) F-0: relationship between load and concrete strain in the compression zone. (<b>b</b>) F-4: relationship between load and concrete strain in the compression zone. (<b>c</b>) F-8: relationship between load and concrete strain in the compression zone.</p>
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<p>Relationship between cumulative residual strain of concrete in the compression zone and the amount of fatigue loading.</p>
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<p>Comparison between calculated and test data curves of cumulative residual strain of concrete in compression zone.</p>
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19 pages, 2160 KiB  
Article
Moderate Highland Barley Intake Affects Anti-Fatigue Capacity in Mice via Metabolism, Anti-Oxidative Effects and Gut Microbiota
by Liangxing Zhao, Qingyu Zhao, Sameh Sharafeldin, Luman Sang, Chao Wang, Yong Xue and Qun Shen
Nutrients 2025, 17(4), 733; https://doi.org/10.3390/nu17040733 - 19 Feb 2025
Viewed by 398
Abstract
Objectives: this study aimed to explore the effects of different intake levels (20–80%) of highland barley on the anti-fatigue capacity of ICR mice, focusing on energy metabolism, metabolite accumulation, oxidative stress, and changes in the gut microbiota. Methods: male ICR mice were assigned [...] Read more.
Objectives: this study aimed to explore the effects of different intake levels (20–80%) of highland barley on the anti-fatigue capacity of ICR mice, focusing on energy metabolism, metabolite accumulation, oxidative stress, and changes in the gut microbiota. Methods: male ICR mice were assigned to five groups: control (normal diet) and four experimental groups with highland barley supplementation at 20%, 40%, 60%, and 80% of total dietary energy. Anti-fatigue performance was assessed by behavioral experiments (rotarod, running, and exhaustive swimming tests), biochemical markers, and gut microbiota analysis. Results: the results showed that moderate supplementation (20%) significantly enhanced exercise endurance and anti-fatigue capacity, as evidenced by increased liver glycogen (134.48%), muscle glycogen (87.75%), ATP content (92.07%), Na+-K+-ATPase activity (48.39%), and antioxidant enzyme activities (superoxide dismutase (103.31%), catalase (87.75%), glutathione peroxidase (81.14%). Post-exercise accumulation of blood lactate, quadriceps muscle lactate, serum urea nitrogen, and the oxidative stress marker malondialdehyde was significantly reduced, with differences of 31.52%, 21.83%, 21.72%, and 33.76%, respectively. Additionally, 20% supplementation promoted the growth of beneficial gut microbiota associated with anti-fatigue effects, including unclassified_f_Lachnospiraceae, g_norank_f_Peptococcaceae, Lachnospiraceae NK4A136, Colidextribacter, and Turicibacter. However, when intake reached 60% or more, anti-fatigue effects diminished, with decreased antioxidant enzyme activity, increased accumulation of metabolic waste, and a rise in potentially harmful microbiota (Allobaculum, Desulfovibrio, and norank_f_norank_o_RF39). Conclusions: moderate highland barley supplementation (20% of total dietary energy) enhances anti-fatigue capacity, while excessive intake (≥60%) may have adverse effects. Full article
(This article belongs to the Special Issue Effects of Dietary Grains on Human Health)
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Figure 1

Figure 1
<p>Experimental Design. Note: (1) normal diet (NC, <span class="html-italic">n</span> = 8) (AIN-93M); (2) normal diet supplemented with 20% highland barley powder (HB20, <span class="html-italic">n</span> = 8); (3) normal diet supplemented with 40% highland barley powder (HB40, <span class="html-italic">n</span> = 8); (4) normal diet supplemented with 60% highland barley powder (HB60, <span class="html-italic">n</span> = 8); (5) normal diet supplemented with 80% highland barley powder (HB80, <span class="html-italic">n</span> = 8).</p>
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<p>Effect of highland barley supplementation on body weight. (<b>A</b>), food intake (g/mouse/day) (<b>B</b>), fatigue measured by time to exhaustion in the rotarod test (<b>C</b>), fatigue measured by time to exhaustion in the treadmill test (<b>D</b>), and fatigue measured by time to exhaustion in the swimming test (<b>E</b>) in mice. Note: In (<b>A</b>,<b>B</b>), statistical comparisons were conducted between groups within the same week, and no significant differences were observed. Bars with different letters (e.g., a, b, c, d) indicate significant differences at <span class="html-italic">p</span> &lt; 0.05. Bars without letters indicate no significant difference.</p>
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<p>Effects of highland barley supplementation on the organ indices of the liver (<b>A</b>), quadriceps (<b>B</b>), and gastrocnemius (<b>C</b>) in mice. Bars with different letters (a, b, c) indicate significant differences at <span class="html-italic">p</span> &lt; 0.05. Note: No significant differences were observed among groups in (<b>A</b>). Bars with different letters (e.g., a, b, c) indicate significant differences at <span class="html-italic">p</span> &lt; 0.05. Bars without letters indicate no significant difference.</p>
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<p>Highland barley supplementation altered the composition of the gut microbiota in mice (<span class="html-italic">n</span> = 6). (<b>A</b>) Shannon index, (<b>B</b>) Simpson index, (<b>C</b>,<b>D</b>) beta diversity, (<b>E</b>) relative abundance at the phylum level, (<b>F</b>) relative abundance at the genus level, (<b>G</b>) Actinobacteriota, Bacteroidota, Cyanobacteria, (<b>H</b>) Firmicutes, Desulfobacterota, Verrucomicrobiota, and (<b>I</b>) Patescibacteria, Proteobacteria, Deferribacterota, Deinococcota. Note: Bars with different letters (e.g., a, b, c) indicate significant differences at <span class="html-italic">p</span> &lt; 0.05. Bars without letters indicate no significant difference.</p>
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<p>(<b>A</b>) <span class="html-italic">Lachnospiraceae_NK4A136_group</span>, <span class="html-italic">norank_f__Muribaculaceae</span>, <span class="html-italic">Allobaculum</span>; (<b>B</b>) <span class="html-italic">unclassified_f__Lachnospiraceae</span>, <span class="html-italic">Akkermansia</span>, <span class="html-italic">Desulfovibrio</span>; (<b>C</b>) <span class="html-italic">Lachnospiraceae_UCG-006</span>, <span class="html-italic">Candidatus_Saccharimonas</span>, <span class="html-italic">Turicibacter</span>; (<b>D</b>) <span class="html-italic">norank_f__Peptococcaceae</span>, <span class="html-italic">norank_f__norank_o__RF39</span>, <span class="html-italic">unclassified_f__Ruminococcaceae</span>; (<b>E</b>) <span class="html-italic">norank_f__Lachnospiraceae</span>, <span class="html-italic">Colidextribacter</span>, <span class="html-italic">Blautia</span>, <span class="html-italic">norank_f__Eubacterium_coprostanoligenes_group</span>; (<b>F</b>) Phylogenetic tree showing the relative abundance of gut microbiota in all groups, with circles representing the phylogenetic levels from phylum (innermost circle) to species (outermost circle). The diameter of each circle is proportional to the abundance of the taxonomic unit; (<b>G</b>) Linear discriminant analysis (LDA) effect size (LEfSe) comparison of gut microbiota in each group with an LDA score &gt; 3. Note: Bars with different letters (e.g., a, b, c) indicate significant differences at <span class="html-italic">p</span> &lt; 0.05. Bars without letters indicate no significant difference.</p>
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<p>Effect of highland barley supplementation on HGB (<b>A</b>), HG (<b>B</b>), LG (<b>C</b>), ATP content in the quadriceps muscle (<b>D</b>), and Na<sup><span class="html-small-caps">+</span></sup>-K<sup>+</sup>-ATPase activity (<b>E</b>) in mice. Note: Bars with different letters (e.g., a, b, c) indicate significant differences at <span class="html-italic">p</span> &lt; 0.05. Bars without letters indicate no significant difference.</p>
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<p>Effect of highland barley supplementation on BUN (<b>A</b>), BLA (<b>B</b>), and LD (<b>C</b>) levels in mice. Note: Bars with different letters (e.g., a, b, c, d) indicate significant differences at <span class="html-italic">p</span> &lt; 0.05. Bars without letters indicate no significant difference.</p>
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<p>Effect of highland barley supplementation on MDA (<b>A</b>), SOD (<b>B</b>), GSH-Px (<b>C</b>), and CAT (<b>D</b>) levels in the liver and on MDA (<b>E</b>), SOD (<b>F</b>), GSH-Px (<b>G</b>), and CAT (<b>H</b>) levels in the quadriceps muscle. Note: Bars with different letters (e.g., a, b, c, d) indicate significant differences at <span class="html-italic">p</span> &lt; 0.05. Bars without letters indicate no significant difference.</p>
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