[go: up one dir, main page]

 
 
Sign in to use this feature.

Years

Between: -

Subjects

remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline

Journals

remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline

Article Types

Countries / Regions

remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline
remove_circle_outline

Search Results (409,111)

Search Parameters:
Keywords = Ising model

Order results
Result details
Results per page
Select all
Export citation of selected articles as:
16 pages, 6178 KiB  
Article
Measurement and Analysis of Carbon Emission Efficiency in the Three Urban Agglomerations of China
by Dan Wu, Xuan Mei and Haili Zhou
Sustainability 2024, 16(20), 9050; https://doi.org/10.3390/su16209050 (registering DOI) - 18 Oct 2024
Abstract
China aims to reduce its carbon emissions to achieve carbon peaking and neutrality. Measuring the carbon emission efficiency of three urban agglomerations in China, exploring their spatiotemporal characteristics, and investigating the main influencing factors are crucial for achieving regional sustainable development and dual [...] Read more.
China aims to reduce its carbon emissions to achieve carbon peaking and neutrality. Measuring the carbon emission efficiency of three urban agglomerations in China, exploring their spatiotemporal characteristics, and investigating the main influencing factors are crucial for achieving regional sustainable development and dual carbon goals. Using the super-slack-based measurement (super-SBM) model, we calculated the carbon emission efficiency of the Beijing–Tianjin–Hebei (BTH), Yangtze River Delta (YRD), and Pearl River Delta (PRD) urban agglomerations from 2011 to 2021 and explored the spatiotemporal non-equilibrium characteristics of carbon emission efficiency and its influencing factors. The results indicated that: (1) Overall, the carbon emission efficiency showed an N-type trend, with the PRD having the highest average efficiency. Regional differences between the YRD and BTH regions gradually increased. (2) The efficiency hotspots shifted from the PRD to the YRD, whereas the cold spots were mainly concentrated in the BTH region. The variation in the standard deviation ellipse radius of carbon emission efficiency in the urban agglomerations was clear, and the spatial disequilibrium was significant. (3) Economic level and opening up had positive impacts on carbon emission efficiency, whereas energy intensity and industrial structure had negative impacts. The effects of population size, government intervention, and technological level varied among the regions. Full article
18 pages, 2434 KiB  
Article
Amine-Terminated Silver Nanoparticles Exhibit Potential for Selective Targeting of Triple-Negative Breast Cancer
by Jayshree H. Ahire, Qi Wang, Yuewei Tao, Yimin Chao and Yongping Bao
Appl. Nano 2024, 5(4), 227-244; https://doi.org/10.3390/applnano5040015 (registering DOI) - 18 Oct 2024
Abstract
Silver nanoparticles (AgNPs) demonstrate potential in treating aggressive cancers such as triple-negative breast cancer (TNBC) in preclinical models. To further the development of AgNP-based therapeutics for clinical use, it is essential to clearly define the specific physicochemical characteristics of the nanoparticles and connect [...] Read more.
Silver nanoparticles (AgNPs) demonstrate potential in treating aggressive cancers such as triple-negative breast cancer (TNBC) in preclinical models. To further the development of AgNP-based therapeutics for clinical use, it is essential to clearly define the specific physicochemical characteristics of the nanoparticles and connect these properties to biological outcomes. This study addresses this knowledge gap through detailed investigations into the structural and surface functional relationships, exploring the mechanisms, safety, and efficacy of AgNPs in targeting TNBC. The surface functionality of nanoparticles is crucial not only for their internalization into cancer cells but also for enhancing their toxicity toward tumor cells. Although the nanoparticles internalized into cancer cells, they failed to exhibit their full toxicity against the cancer. Herein we report a solvent-assisted synthesis amine, mercaptohexanol and bifunctional silver nanoparticles and performing comparative study to understand their selectivity and toxicity toward TNBC cells. The nanoparticles are fully characterized by UV–visible absorption spectroscopy, Fourier transform infrared spectroscopy (FTIR), scanning electron microscopy (SEM), and dynamic light scattering measurement (DLS). The synthesis method achieves an extremely high yield and surface coating ratio of synthesized colloidal AgNPs. Our findings reveal that the amine-capped AgNPs exhibit significant selective toxicity against TNBC cell lines MCF7 and MDA-MB-231 at a concentration of 40 µg/mL without affecting normal breast cell lines MCF10A. This study underscores the potential of functionalized AgNPs in developing safe and targeted therapeutic approaches for treating aggressive cancers like TNBC, laying the groundwork for future clinical advancements. Full article
(This article belongs to the Collection Feature Papers for Applied Nano)
Show Figures

Figure 1

Figure 1
<p>The UV–vis spectra displayed above provide insights into the optical properties of Cyst-AgNPs (red), MH-AgNPs (blue), and MH+cyst-AgNPs (green) when suspended in water. These spectra are instrumental in understanding the formation and stability of the nanoparticles, as well as their surface plasmon resonance (SPR) characteristics.</p>
Full article ">Figure 2
<p>The Fourier transform infrared (FTIR) spectra presented above illustrate the functional groups and molecular interactions associated with (<b>a</b>) Cyst-AgNPs, (<b>b</b>) MH-AgNPs, and (<b>c</b>) MH+cyst-AgNPs. The ATR spectra of purified solid samples showing the comparison of functionalized silver nanoparticles with their respective capping agents: cysteamine hydrochloride, mercapto hexanol and combination of both. The spectra were normalized with respect to the 1589 cm<sup>−1</sup> peak. The blue columns indicate the region corresponding to thiol functionality.</p>
Full article ">Figure 2 Cont.
<p>The Fourier transform infrared (FTIR) spectra presented above illustrate the functional groups and molecular interactions associated with (<b>a</b>) Cyst-AgNPs, (<b>b</b>) MH-AgNPs, and (<b>c</b>) MH+cyst-AgNPs. The ATR spectra of purified solid samples showing the comparison of functionalized silver nanoparticles with their respective capping agents: cysteamine hydrochloride, mercapto hexanol and combination of both. The spectra were normalized with respect to the 1589 cm<sup>−1</sup> peak. The blue columns indicate the region corresponding to thiol functionality.</p>
Full article ">Figure 3
<p>Showing the scanning electron microscopy (SEM) images of silver nanoparticles (<b>a</b>) Cyst-AgNPs, (<b>b</b>) MH-AgNPs, and (<b>c</b>) MH+cyst-AgNPs. Below is a respective histogram of the nanoparticles displaying the size distribution and mean diameter of the synthesized nanoparticles.</p>
Full article ">Figure 4
<p>The energy-dispersive spectroscopy (EDS) showing a comprehensive analysis of the elemental composition of three types of silver nanoparticles: (<b>a</b>) Cyst-AgNPs, (<b>b</b>) MH-AgNPs, and (<b>c</b>) MH+cyst-AgNPs.</p>
Full article ">Figure 5
<p>Displays the dynamic light scattering (DLS) spectra for three types of silver nanoparticles: Cyst-AgNPs (red), MH-AgNPs (blue), and MH+cyst-AgNPs (green) when dispersed in water. The spectra provide insights into the size distribution and stability of the nanoparticles in an aqueous environment.</p>
Full article ">Figure 6
<p>Illustrates the zeta potential of silver nanoparticles measured in water at three different pH levels: acidic (pH 3), neutral (pH 7), and alkaline (pH 10). The zeta potential values indicate the surface charge of the nanoparticles, which plays a critical role in their stability and interactions in biological systems.</p>
Full article ">Figure 7
<p>Presents the results of a cell viability assay evaluating the dose dependent toxicity effects of different silver nanoparticles on breast cancer cell lines MCF10A and MDA-MB-231, as well as normal breast cells (MCF-7). There are significant differences among all three cell lines, <span class="html-italic">p</span>-value &lt; 0.001.</p>
Full article ">Scheme 1
<p>Schematic representation of synthesis of Cyst-AgNPs, MH+cyst-AgNPs and MH-AgNPs.</p>
Full article ">
10 pages, 433 KiB  
Article
The Impact of Social Participation on Frailty Among Older Adults: The Mediating Role of Loneliness and Sleep Quality
by Yanting Wang, Feiyang Zheng and Xinping Zhang
Healthcare 2024, 12(20), 2085; https://doi.org/10.3390/healthcare12202085 (registering DOI) - 18 Oct 2024
Abstract
Background: Frailty has become a common health issue among older adults, imposing a burden on both society and individuals. The relationship between social participation and frailty has received widespread attention, but the mechanism remains to be explored. The aim of this study is [...] Read more.
Background: Frailty has become a common health issue among older adults, imposing a burden on both society and individuals. The relationship between social participation and frailty has received widespread attention, but the mechanism remains to be explored. The aim of this study is to explore the impact of social participation on frailty among older adults and to analyze the mediating role of loneliness and sleep quality, providing suggestions to alleviate frailty. Methods: Data related to social participation, loneliness, sleep quality, and frailty from 7779 older adults were collected from the Chinese Longitudinal Healthy Longevity Survey (CLHLS 2018). The chain mediation model was conducted to explore the relationship between variables, and the Bootstrap method was used to examine the path coefficients. Results: Social participation negatively affected frailty (β = −0.00391049, 95% CI = [−0.042296, −0.035465]); the indirect effect of social participation on frailty mediated by loneliness was −0.0019505 (95% CI = [−0.002551, −0.001371]); the indirect effect of social participation on frailty mediated by sleep quality was −0.0011104 (95%CI = [−0.001692, −0.000557]); the effect mediated by both loneliness and sleep quality was −0.0004263 (95% CI = [−0.000593, −0.000304]). Conclusions: Social participation negatively affected frailty. Loneliness and sleep quality not only mediated independently, but also played a chain mediating role. This suggested that encouraging older adults to engage in more social participation, reducing loneliness, and improving sleep quality are feasible measures to improve frailty. Full article
62 pages, 5893 KiB  
Article
Simulation-Based Design for Recycling of Car Electronic Modules as a Function of Disassembly Strategies
by Antoinette van Schaik and Markus A. Reuter
Sustainability 2024, 16(20), 9048; https://doi.org/10.3390/su16209048 (registering DOI) - 18 Oct 2024
Abstract
Modules (or parts) of a car are a complex functional material combination used to deliver a specified task for a car. Recovering all materials, energy, etc., into high-grade materials at their end of life (EoL) is impossible. This is dictated by the second [...] Read more.
Modules (or parts) of a car are a complex functional material combination used to deliver a specified task for a car. Recovering all materials, energy, etc., into high-grade materials at their end of life (EoL) is impossible. This is dictated by the second law of thermodynamics (2LT) and thence economics. Thus, recyclability cannot be conducted with simplistic mass-based approaches void of thermodynamic considerations. We apply, in this paper, a process simulation model to estimate the true recyclability of various SEAT (Volkswagen Group) car parts within the EU H2020 TREASURE project. This simulation model is developed with 190 reactors and over 310 feed components with over 1000 reaction species in the 880 streams of the flowsheet. The uniqueness of the work in this paper is to apply the full material declaration (FMD) and bill of materials (BOM) of all 310 materials in the parts as a feed to the process simulation model to show the parts’ true recyclability. We classified all parts into categories, i.e., copper-rich, steel-rich and plastic-rich, to maximally recover metals at the desired material quality, as well as energy. Recyclability is understood to create high-grade products that can be applied with the same functional quality in these parts. In addition, disassembly strategies and related possible redesign show how much recyclability can be improved. Process simulation permits the creation of alloys, phases, materials, etc., at a desired quality. The strength of the simulation permits any feed from any End-of-Life part to be analyzed, as long as the FMD and BOM are available. This is analogous to any mineral and metallurgical engineering process simulation for which the full mineralogy must be available to analyze and/or design flowsheets. This paper delivers a wealth of data for various parts as well as the ultimate recovery of materials, elements, and energy. The results show clearly that there is no one single recycling rate for elements, materials, and alloys. It is in fact a function of the complexity and material combinations within the parts. The fact that we use a thermochemical-based process simulator with full compositional detail for the considered parts means full energy balances as well as exergy dissipation can be evaluated. This means that we can also evaluate which parts, due complex mixtures of plastics, are best processed for energy recovery or are best for material and metal recovery, with thermochemistry, reactor technology and integrated flowsheets being the basis. Full article
15 pages, 1084 KiB  
Article
Machine Learning Model Trained with Finite Element Modeling Can Predict the Risk of Osteoarthritis: Data from the Osteoarthritis Initiative
by Mika E. Mononen, Mimmi K. Liukkonen and Mikael J. Turunen
Appl. Sci. 2024, 14(20), 9538; https://doi.org/10.3390/app14209538 (registering DOI) - 18 Oct 2024
Abstract
Objective: Despite long simulation times, recently developed finite element analysis (FEA) models of knee joints have demonstrated their suitability for predicting individual risk of onset and progression of knee osteoarthritis. Therefore, the objective of this study was to assess the feasibility of machine [...] Read more.
Objective: Despite long simulation times, recently developed finite element analysis (FEA) models of knee joints have demonstrated their suitability for predicting individual risk of onset and progression of knee osteoarthritis. Therefore, the objective of this study was to assess the feasibility of machine learning (ML) to replicate outcomes obtained from FEA when simulating mechanical responses and predicting cartilage degeneration within the knee joint.Design: Two ML models based on the Gaussian Process Regression (GPR) algorithms were developed. The first model (GPR1) utilized age, weight, and anatomical joint dimensions as predictor variables to predict tissue mechanical responses and cartilage degeneration based on FEA data. The second model (GPR2) utilized age, weight, height, and gender to predict anatomical joint dimensions, which were then used as inputs in the GPR1 model. Finally, the GPR1 and combined GPR1+GPR2 models were used to investigate the importance of clinical imaging when making personalized predictions for knees from healthy subjects with no history of knee injuries.Results: In the GPR1 model, R2 of 0.9 was exceeded for most of the predicted mechanical parameters. The GPR2 model was able to predict knee shape with R2 of 0.67–0.9. Both GPR1 and combined GPR1+GPR2 models offered equally good performances (AUC = 0.73–0.74) in classifying patients at high risk for the onset and development of knee osteoarthritis.Conclusions: In the future, real-time and easy-to-use GPR models may provide a rapid technology to evaluate mechanical responses within the knee for researchers or clinicians who have no former knowledge of FEA. Full article
(This article belongs to the Section Biomedical Engineering)
15 pages, 3652 KiB  
Article
Dual-Modal Illumination System for Defect Detection of Aircraft Glass Canopies
by Zijian Li, Yong Yao, Runyuan Wen and Qiyang Liu
Sensors 2024, 24(20), 6717; https://doi.org/10.3390/s24206717 (registering DOI) - 18 Oct 2024
Abstract
Defect detection in transparent materials typically relies on specific lighting conditions. However, through our work on defect detection for aircraft glass canopies, we found that using a single lighting condition often led to missed or false detections. This limitation arises from the optical [...] Read more.
Defect detection in transparent materials typically relies on specific lighting conditions. However, through our work on defect detection for aircraft glass canopies, we found that using a single lighting condition often led to missed or false detections. This limitation arises from the optical properties of transparent materials, where certain defects only become sufficiently visible under specific lighting angles. To address this issue, we developed a dual-modal illumination system that integrates both forward and backward lighting to capture defect images. Additionally, we introduced the first dual-modal dataset for defect detection in aircraft glass canopies. Furthermore, we proposed an attention-based dual-branch modal fusion network (ADMF-Net) to enhance the detection process. Experimental results show that our system and model significantly improve the detection performance, with the dual-modal approach increasing the mAP by 5.6% over the single-modal baseline, achieving a mAP of 98.4%. Our research also provides valuable insights for defect detection in other transparent materials. Full article
(This article belongs to the Special Issue Deep-Learning-Based Defect Detection for Smart Manufacturing)
Show Figures

Figure 1

Figure 1
<p>Schematic diagram of the light path of common illumination structures. (<b>a</b>) Bright field and dark field forward lighting. (<b>b</b>) Scattering forward lighting. (<b>c</b>) Backward lighting.</p>
Full article ">Figure 2
<p>Typical defect samples under different illumination structures.</p>
Full article ">Figure 3
<p>Prototype dual-modal illumination image acquisition platform.</p>
Full article ">Figure 4
<p>Forward lighting and backward lighting implementation.</p>
Full article ">Figure 5
<p>Aircraft glass canopy samples.</p>
Full article ">Figure 6
<p>Typical images of four types of defects.</p>
Full article ">Figure 7
<p>RGB Channel Fusion method.</p>
Full article ">Figure 8
<p>The architecture of the proposed ADMF-Net.</p>
Full article ">Figure 9
<p>A comparison of the two proposed methods. First row: RGB Channel Fusion. Second row: ADMF-Net.</p>
Full article ">Figure 10
<p>Normalized confusion matrix of single lighting methods and our fusion methods. (<b>a</b>) Forward lighting. (<b>b</b>) Backward lighting. (<b>c</b>) RGB Channel Fusion. (<b>d</b>) ADMF-Net.</p>
Full article ">
25 pages, 5517 KiB  
Article
Gust Response and Alleviation of Avian-Inspired In-Plane Folding Wings
by Haibo Zhang, Haolin Yang, Yongjian Yang, Chen Song and Chao Yang
Biomimetics 2024, 9(10), 641; https://doi.org/10.3390/biomimetics9100641 (registering DOI) - 18 Oct 2024
Abstract
The in-plane folding wing is one of the important research directions in the field of morphing or bionic aircraft, showing the unique application value of enhancing aircraft maneuverability and gust resistance. This article provides a structural realization of an in-plane folding wing and [...] Read more.
The in-plane folding wing is one of the important research directions in the field of morphing or bionic aircraft, showing the unique application value of enhancing aircraft maneuverability and gust resistance. This article provides a structural realization of an in-plane folding wing and an aeroelasticity modeling method for the folding process of the wing. By approximating the change in structural properties in each time step, a method for calculating the structural transient response expressed in recursive form is obtained. On this basis, an aeroelasticity model of the wing is developed by coupling with the aerodynamic model using the unsteady panel/viscous vortex particle hybrid method. A wind-tunnel test is implemented to demonstrate the controllable morphing capability of the wing under aerodynamic loads and to validate the reliability of the wing loads predicted by the method in this paper. The results of the gust simulation show that the gust scale has a significant effect on the response of both the open- and closed-loop systems. When the gust alleviation controller is enabled, the peak bending moment at the wing root can be reduced by 5.5%∼47.3% according to different gust scales. Full article
Show Figures

Figure 1

Figure 1
<p>Scheme of the in-plane folding wing.</p>
Full article ">Figure 2
<p>Cross-section shape of the wing.</p>
Full article ">Figure 3
<p>Design of skeleton-inspired beam.</p>
Full article ">Figure 4
<p>Iteration process for optimization design.</p>
Full article ">Figure 5
<p>Optimized result of cross-section radius distribution of rods in cells.</p>
Full article ">Figure 6
<p>Beam with cellular structure of non-uniform density.</p>
Full article ">Figure 7
<p>Prototype of avian-inspired in-plane folding wing. (<b>a</b>) Skeleton only. (<b>b</b>) Skin is attached.</p>
Full article ">Figure 8
<p>Parameter approximating within a single time step. (<b>a</b>) Hermite interpolation for structural parameters. (<b>b</b>) Linear interpolation for generalized coordinates.</p>
Full article ">Figure 9
<p>Unsteady panel/viscous vortex particle hybrid method.</p>
Full article ">Figure 10
<p>Coupling workflows of aeroelasticity model of in-plane folding wings.</p>
Full article ">Figure 11
<p>Wind-tunnel test of the wing prototype.</p>
Full article ">Figure 12
<p>Comparison of the wing loads at the steady working condition (<math display="inline"><semantics> <mrow> <mi>u</mi> <mo>=</mo> <mn>10</mn> </mrow> </semantics></math> ms<math display="inline"><semantics> <msup> <mo>⁢</mo> <mrow> <mo>−</mo> <mn>1</mn> </mrow> </msup> </semantics></math>, <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <msup> <mn>5</mn> <mo>∘</mo> </msup> </mrow> </semantics></math>). (<b>a</b>) Lift. (<b>b</b>) Drag and lift-to-drag ratio.</p>
Full article ">Figure 13
<p>Comparison of the wing lift results at the unsteady working condition (<math display="inline"><semantics> <mrow> <mi>u</mi> <mo>=</mo> <mn>10</mn> </mrow> </semantics></math> ms<math display="inline"><semantics> <msup> <mo>⁢</mo> <mrow> <mo>−</mo> <mn>1</mn> </mrow> </msup> </semantics></math>, <math display="inline"><semantics> <mrow> <mi>α</mi> <mo>=</mo> <msup> <mn>5</mn> <mo>∘</mo> </msup> </mrow> </semantics></math>, <math display="inline"><semantics> <mrow> <mi>f</mi> <mo>=</mo> <mn>0.5</mn> </mrow> </semantics></math> Hz).</p>
Full article ">Figure 14
<p>Gust field velocity curve.</p>
Full article ">Figure 15
<p>Bending moment at the wing root.</p>
Full article ">Figure 16
<p>Comparison of the dynamic and quasi-static models. (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>λ</mi> <mo>=</mo> <mn>2</mn> <mi>c</mi> </mrow> </semantics></math>, dynamic model. (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>λ</mi> <mo>=</mo> <mn>2</mn> <mi>c</mi> </mrow> </semantics></math>, quasi-static model. (<b>c</b>) <math display="inline"><semantics> <mrow> <mi>λ</mi> <mo>=</mo> <mn>80</mn> <mi>c</mi> </mrow> </semantics></math>, dynamic model. (<b>d</b>) <math display="inline"><semantics> <mrow> <mi>λ</mi> <mo>=</mo> <mn>80</mn> <mi>c</mi> </mrow> </semantics></math>, quasi-static model.</p>
Full article ">Figure 17
<p>Maximum additional bending moment at the wing root.</p>
Full article ">Figure 18
<p>Wing aeroservoelastic system schematic.</p>
Full article ">Figure 19
<p>Servo system schematic.</p>
Full article ">Figure 20
<p>Gust alleviation controller schematic.</p>
Full article ">Figure 21
<p>Designing of gust alleviation controller.</p>
Full article ">Figure 22
<p>Bending moment response curve of the closed-loop system. (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>λ</mi> <mo>=</mo> <mn>2</mn> <mi>c</mi> </mrow> </semantics></math>, comparison of additional bending moments. (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>λ</mi> <mo>=</mo> <mn>2</mn> <mi>c</mi> </mrow> </semantics></math>, variation of folding angle. (<b>c</b>) <math display="inline"><semantics> <mrow> <mi>λ</mi> <mo>=</mo> <mn>9</mn> <mi>c</mi> </mrow> </semantics></math>, comparison of additional bending moments. (<b>d</b>) <math display="inline"><semantics> <mrow> <mi>λ</mi> <mo>=</mo> <mn>9</mn> <mi>c</mi> </mrow> </semantics></math>, variation of folding angle. (<b>e</b>) <math display="inline"><semantics> <mrow> <mi>λ</mi> <mo>=</mo> <mn>80</mn> <mi>c</mi> </mrow> </semantics></math>, comparison of additional bending moments. (<b>f</b>) <math display="inline"><semantics> <mrow> <mi>λ</mi> <mo>=</mo> <mn>80</mn> <mi>c</mi> </mrow> </semantics></math>, variation of folding angle.</p>
Full article ">Figure 23
<p>Effect of the controller under different scales of gusts.</p>
Full article ">
24 pages, 3101 KiB  
Article
Combined Freak Wave, Wind, and Current Effects on the Dynamic Responses of Offshore Triceratops
by Nagavinothini Ravichandran
J. Mar. Sci. Eng. 2024, 12(10), 1876; https://doi.org/10.3390/jmse12101876 (registering DOI) - 18 Oct 2024
Abstract
Offshore structures are exposed to various environmental loads, including extreme and abnormal waves, over their operational lifespan. The existence of wind and current can exacerbate the dynamic response of these structures, posing threats to safety and integrity. This study focuses on the dynamic [...] Read more.
Offshore structures are exposed to various environmental loads, including extreme and abnormal waves, over their operational lifespan. The existence of wind and current can exacerbate the dynamic response of these structures, posing threats to safety and integrity. This study focuses on the dynamic responses of offshore triceratops under different environmental conditions characterized by the superimposition of freak waves, uniform wind, and current. The free surface profile of the freak wave was generated using the dual superposition model. The numerical model of the offshore platform designed for ultra-deep-water applications was developed using the ANSYS AQWA 2023 R2 modeler. Numerical investigations, including the free decay tests and time-domain analysis under random sea states, including freak waves, were initially carried out. Then, the combined effects of freak waves, wind, and current were studied in detail under different loading scenarios. The results revealed the increase in structural response under the freak wave action at the focus time. Wind action resulted in a mean shift in responses, while the inclusion of current led to a pronounced increase in the total response of the platform, encompassing deck and buoyant legs, alongside the tether tension variation. Notably, considerable variations in the response were observed after freak wave exposure under the combined influence of wind, freak wave, and current. The results underscore the profound effects induced by wind and current in the presence of freak waves, providing valuable insights for analyzing similar offshore structures under ultimate design conditions. Full article
39 pages, 35650 KiB  
Article
An Analysis of a Complete Aircraft Electrical Power System Simulation Based on a Constant Speed Constant Frequency Configuration
by Octavian Grigore-Müler
Aerospace 2024, 11(10), 860; https://doi.org/10.3390/aerospace11100860 (registering DOI) - 18 Oct 2024
Abstract
Recent developments in aircraft electrical technology, such as the design and production of more electric aircraft (MEA) and major steps in the development of all-electric aircraft (AEA), have had a significant impact on aircraft’ electrical power systems (EPSs). However, the EPSs of the [...] Read more.
Recent developments in aircraft electrical technology, such as the design and production of more electric aircraft (MEA) and major steps in the development of all-electric aircraft (AEA), have had a significant impact on aircraft’ electrical power systems (EPSs). However, the EPSs of the latest aircraft produced by the main players in the market, Airbus with the Neo series and Boeing with the NG and MAX series are still completely traditional and based on the constant speed constant frequency (CSCF) configuration. For alternating current ones, the EPS is composed of the following: prime movers, namely the aircraft turbofan engine (TE); the electrical power source, i.e., the integrated drive generator (IDG); the command and control system, the generator control unit (GCU); the transmission and the system distribution system; the protection system, i.e., the CBs (circuit breakers); and the electrical loads. This paper presents the analysis of this system using the Simscape package from Simulink v 8.7, a MATLAB v 9.0 program, which is actually the development of some systems designed in two previous personal papers. For the first time in the literature, a complete MATLAB modelled EPS system was presented, i.e., the aircraft turbofan engine model, driven by the constant speed drive system (CSD) (model presented in the first reference as a standalone type and with different parameters), linked to the synchronous generator (SG) (model presented in second reference for lower power and rotational speed) in the so-called integrated drive generator (IDG) and electrical loads. Full article
(This article belongs to the Special Issue Electric Power Systems and Components for All-Electric Aircraft)
Show Figures

Figure 1

Figure 1
<p>The typical EPS configurations [<a href="#B2-aerospace-11-00860" class="html-bibr">2</a>].</p>
Full article ">Figure 2
<p>The total number of commercial airplane MEA and non-MEA in service in 2024 (data from [<a href="#B15-aerospace-11-00860" class="html-bibr">15</a>]).</p>
Full article ">Figure 3
<p>The EPS architecture of a CSCF AC configuration [<a href="#B2-aerospace-11-00860" class="html-bibr">2</a>].</p>
Full article ">Figure 4
<p>Schematic representation of a gas turbine engine with a control volume around it to determine the thrust.</p>
Full article ">Figure 5
<p>The block diagram of IDGS and governor system [<a href="#B2-aerospace-11-00860" class="html-bibr">2</a>]: 1—centrifugal transducer; 2—measuring device (distributor)—two-way spool valve; 3—calibrating device (spring); 4—device for tuning centrifugal element; 5—hydraulic servomotor; 6—feedback mechanism.</p>
Full article ">Figure 6
<p>Sketch of a differential hydraulic CSD [<a href="#B1-aerospace-11-00860" class="html-bibr">1</a>]; P—pump; G—gear box; OT—oil tank; 1—hydraulic actuator; 2—centrifugal transducer; 3—piston; 4—fixed disc of FHU; 5—FHU rotor; 6—the mechanical differential planetary gear; 7—the suction washer of the suction and discharge channels (distribution element); 8—variable angle wobbler of VHU (swash plate); 9—VHU rotor; 10—the distributor.</p>
Full article ">Figure 7
<p>Sketch of the forces acting on CSD fixed disc [<a href="#B1-aerospace-11-00860" class="html-bibr">1</a>].</p>
Full article ">Figure 8
<p>Components of a modern BSG [<a href="#B2-aerospace-11-00860" class="html-bibr">2</a>]: <span class="html-italic">PE</span>—pilot exciter, a 3-ph <span class="html-italic">SG</span> with permanent magnet (<span class="html-italic">PMG</span>); <span class="html-italic">E</span>—exciter, a 3-ph <span class="html-italic">SG</span> of inverted construction; <span class="html-italic">RR</span>—rotary rectifier.</p>
Full article ">Figure 9
<p>SG phase-variable circuit model [<a href="#B2-aerospace-11-00860" class="html-bibr">2</a>]; <span class="html-italic">a</span>, <span class="html-italic">b</span>, <span class="html-italic">c</span>—stator phase windings; <span class="html-italic">fd</span>—field winding; <span class="html-italic">kd</span>—<span class="html-italic">d</span>-axis dumper circuit; <span class="html-italic">kq</span>—<span class="html-italic">q</span>-axis dumper circuit; <span class="html-italic">k</span> = 1, n, n—number pf dumper circuits; <span class="html-italic">θ</span>—angle by which <span class="html-italic">d</span>-axis leads the magnetic axis of phase <span class="html-italic">a</span> winding; <span class="html-italic">ω</span><sub>r</sub>—rotor angular speed.</p>
Full article ">Figure 10
<p>The RSR diagram [<a href="#B2-aerospace-11-00860" class="html-bibr">2</a>].</p>
Full article ">Figure 11
<p>Diagram of the driven generator model [<a href="#B2-aerospace-11-00860" class="html-bibr">2</a>].</p>
Full article ">Figure 12
<p>The control of a BSG [<a href="#B2-aerospace-11-00860" class="html-bibr">2</a>,<a href="#B48-aerospace-11-00860" class="html-bibr">48</a>].</p>
Full article ">Figure 13
<p>Type AC1A alternator rectifier excitation system with noncontrolled rectifiers and feedback from exciter field current [<a href="#B48-aerospace-11-00860" class="html-bibr">48</a>].</p>
Full article ">Figure 14
<p>Aircraft electrical power generation and distribution system Simulink model.</p>
Full article ">Figure 15
<p>Simulink model for aircraft turbofan engine.</p>
Full article ">Figure 16
<p>Variation of the aircraft turbofan engine characteristics.</p>
Full article ">Figure 17
<p>Simulink model for accessory gearbox.</p>
Full article ">Figure 18
<p>Variation of the accessory gearbox characteristics.</p>
Full article ">Figure 19
<p>Simulink model for IDGS.</p>
Full article ">Figure 20
<p>The Simulink model parameters.</p>
Full article ">Figure 21
<p>Simulink model for CSD.</p>
Full article ">Figure 22
<p>Variation of the CSD characteristics without AFR.</p>
Full article ">Figure 23
<p>Shape of the output characteristics of the CSD.</p>
Full article ">Figure 23 Cont.
<p>Shape of the output characteristics of the CSD.</p>
Full article ">Figure 24
<p>Simulink model for BSG.</p>
Full article ">Figure 25
<p>Main characteristics of synchronous generator.</p>
Full article ">Figure 26
<p>Simulink model for GCU [<a href="#B2-aerospace-11-00860" class="html-bibr">2</a>].</p>
Full article ">Figure 27
<p>PID parameters.</p>
Full article ">Figure 28
<p>Variation of the CSD characteristics with AFR.</p>
Full article ">Figure 29
<p>Variation of the BSG frequency compared to the limits in the standard (data limits from [<a href="#B45-aerospace-11-00860" class="html-bibr">45</a>]).</p>
Full article ">Figure 30
<p>Variation of the BSG terminal parameters compared to the limits in the standard [<a href="#B45-aerospace-11-00860" class="html-bibr">45</a>].</p>
Full article ">Figure 31
<p>Variation of the BSG exciter output voltage.</p>
Full article ">Figure 32
<p>Variation of the accessory gearbox characteristics: (<b>a</b>) for GOL scenario; (<b>b</b>) for ICL scenario.</p>
Full article ">Figure 33
<p>Variation of the CSD characteristics: (<b>a</b>) for GOL scenario; (<b>b</b>) for ICL scenario.</p>
Full article ">Figure 34
<p>Variation of the BSG frequency compared to the limits in the standard (data limits from [<a href="#B45-aerospace-11-00860" class="html-bibr">45</a>]): (<b>a</b>) for GOL scenario; (<b>b</b>) for ICL scenario.</p>
Full article ">Figure 35
<p>Variation of the BSG characteristics compared to the limits in the standard (data limits from [<a href="#B45-aerospace-11-00860" class="html-bibr">45</a>]) for GOL scenario.</p>
Full article ">Figure 36
<p>Variation of the BSG exciter output voltage: (<b>a</b>) for GOL scenario; (<b>b</b>) for ICL scenario.</p>
Full article ">Figure 37
<p>Variation of the BSG characteristics compared to the limits in the standard (data limits from [<a href="#B45-aerospace-11-00860" class="html-bibr">45</a>]) for ICL scenario.</p>
Full article ">
28 pages, 1310 KiB  
Article
Non-Periodic Quantized Model Predictive Control Method for Underwater Dynamic Docking
by Tian Ni, Can Sima, Liang Qi, Minghao Xu, Junlin Wang, Runkang Tang and Lindan Zhang
Symmetry 2024, 16(10), 1392; https://doi.org/10.3390/sym16101392 (registering DOI) - 18 Oct 2024
Abstract
This study proposed an event-triggered quantized model predictive control (ETQMPC) method for the dynamic docking of unmanned underwater vehicles (UUVs) and human-occupied vehicles (HOVs). The proposed strategy employed a non-periodic control approach that initiated the non-linear model predictive control (NMPC) optimization and state [...] Read more.
This study proposed an event-triggered quantized model predictive control (ETQMPC) method for the dynamic docking of unmanned underwater vehicles (UUVs) and human-occupied vehicles (HOVs). The proposed strategy employed a non-periodic control approach that initiated the non-linear model predictive control (NMPC) optimization and state sampling based on tracking errors and deviations from the predicted optimal state, thereby enhancing computing performance and system efficiency without compromising the control quality. To further conserve communication resources and improve information transfer efficiency, a quantitative feedback mechanism was employed for sampling and state quantification. The simulation experiments were performed to verify the effectiveness of the method, demonstrating excellent docking trajectory tracking performance, robustness against bounded current interference, and significant reductions in computational and communication burdens. The experimental results demonstrated that the method outperformed in the docking trajectory tracking control performance significantly improved the computational and communication performance, and comprehensively improved the system efficiency. Full article
(This article belongs to the Special Issue Symmetry in Control System Theory and Applications)
9 pages, 1385 KiB  
Communication
Discovery of Anti-Inflammatory Alkaloids from Sponge Stylissa massa Suggests New Biosynthetic Pathways for Pyrrole–Imidazole Alkaloids
by Xiaojing Liu, Qi Wang, Yun Zhang and Hanting Zhang
Mar. Drugs 2024, 22(10), 477; https://doi.org/10.3390/md22100477 (registering DOI) - 18 Oct 2024
Abstract
Pyrrole–imidazole alkaloids (PIAs) are a class of marine sponge derived natural products which have complex carbon frameworks and broad bioactivities. In this study, four new alkaloids, stylimassalins A–B (12), 3, and 5, together with two known compounds [...] Read more.
Pyrrole–imidazole alkaloids (PIAs) are a class of marine sponge derived natural products which have complex carbon frameworks and broad bioactivities. In this study, four new alkaloids, stylimassalins A–B (12), 3, and 5, together with two known compounds (4 and 6), were isolated from Stylissa massa. Compounds 2, 4, and 6 are the C-2 brominated analogues of 1, 3, and 5, respectively. Their structures display three different scaffolds, of which scaffold 1 (compounds 1,2) is new. A new biosynthetic pathway from oroidin, through spongiacidin, to latonduine and scaffold 1 was proposed by our group, in which the C12-N13-cleavaged compounds of spongiacidin (scaffold 2), dubbed seco-spongiacidins (3 and 4), are recognized as a key bridged scaffold, to afford PIA analogues (1,2 and 5,6). An anti-inflammatory evaluation in a zebrafish inflammation model induced by copper sulphate (CuSO4) demonstrated that stylimassalins A and B (1 and 2) could serve as a promising lead scaffold for treating inflammation. Full article
(This article belongs to the Special Issue Bio-Active Components from Marine Sponges)
12 pages, 1532 KiB  
Article
Predicting Invasiveness in Lepidic Pattern Adenocarcinoma of Lung: Analysis of Visual Semantic and Radiomic Features
by Sean F. Johnson, Seyed Mohammad Hossein Tabatabaei, Grace Hyun J. Kim, Bianca E. Villegas, Matthew Brown, Scott Genshaft, Robert D. Suh, Igor Barjaktarevic, William Dean Wallace and Fereidoun Abtin
Med. Sci. 2024, 12(4), 57; https://doi.org/10.3390/medsci12040057 (registering DOI) - 18 Oct 2024
Abstract
Objectives: To differentiate invasive lepidic predominant adenocarcinoma (iLPA) from adenocarcinoma in situ (AIS)/minimally invasive adenocarcinoma (MIA) of lung utilizing visual semantic and computer-aided detection (CAD)-based texture features on subjects initially diagnosed as AIS or MIA with CT-guided biopsy. Materials and Methods: From 2011 [...] Read more.
Objectives: To differentiate invasive lepidic predominant adenocarcinoma (iLPA) from adenocarcinoma in situ (AIS)/minimally invasive adenocarcinoma (MIA) of lung utilizing visual semantic and computer-aided detection (CAD)-based texture features on subjects initially diagnosed as AIS or MIA with CT-guided biopsy. Materials and Methods: From 2011 to 2017, all patients with CT-guided biopsy results of AIS or MIA who subsequently underwent resection were identified. CT scan before the biopsy was used to assess visual semantic and CAD texture features, totaling 23 semantic and 95 CAD-based quantitative texture variables. The least absolute shrinkage and selection operator (LASSO) method or forward selection was used to select the most predictive feature and combination of semantic and texture features for detection of invasive lung adenocarcinoma. Results: Among the 33 core needle-biopsied patients with AIS/MIA pathology, 24 (72.7%) had invasive LPA and 9 (27.3%) had AIS/MIA on resection. On CT, visual semantic features included 21 (63.6%) part-solid, 5 (15.2%) pure ground glass, and 7 (21.2%) solid nodules. LASSO selected seven variables for the model, but all were not statistically significant. “Volume” was found to be statistically significant when assessing the correlation between independent variables using the backward selection technique. The LASSO selected “tumor_Perc95”, “nodule surround”, “small cyst-like spaces”, and “volume” when assessing the correlation between independent variables. Conclusions: Lung biopsy results showing noninvasive LPA underestimate invasiveness. Although statistically non-significant, some semantic features showed potential for predicting invasiveness, with septal stretching absent in all noninvasive cases, and solid consistency present in a significant portion of invasive cases. Full article
(This article belongs to the Section Cancer and Cancer-Related Research)
21 pages, 6957 KiB  
Article
Inversion Method for Material Parameters of Concrete Dams Using Intelligent Algorithm-Based Displacement Separation
by Jianrong Xu, Lingang Gao, Tongchun Li, Jinhua Guo, Huijun Qi, Yu Peng and Jianxin Wang
Water 2024, 16(20), 2979; https://doi.org/10.3390/w16202979 (registering DOI) - 18 Oct 2024
Abstract
Integrating long-term observational data analysis with numerical simulations of dam operations provides an effective approach to dam safety evaluation. However, analytical results are often subject to errors due to challenges in accurately surveying and modeling the foundation, as well as temporal changes in [...] Read more.
Integrating long-term observational data analysis with numerical simulations of dam operations provides an effective approach to dam safety evaluation. However, analytical results are often subject to errors due to challenges in accurately surveying and modeling the foundation, as well as temporal changes in foundation properties. This paper proposes a concrete dam displacement separation model that distinguishes between deformation caused by foundation restraint and that induced by external loads. By combining this model with intelligent optimization techniques and long-term observational data, we can identify the actual mechanical parameters of the dam and conduct structural health assessments. The proposed model accommodates multiple degrees of freedom and is applicable to both two- and three-dimensional dam modeling. Consequently, it is well-suited for parameter identification and health diagnosis of concrete gravity and arch dams with extensive observational data. The efficacy of this diagnostic model has been validated through computational case studies and practical engineering applications. Full article
Show Figures

Figure 1

Figure 1
<p>Simplified dam–foundation system using virtual springs for 2D and 3D models.</p>
Full article ">Figure 2
<p>Hierarchy of grey wolf (dominance decreases from top down).</p>
Full article ">Figure 3
<p>The flowchart of intelligent inversion of parameters.</p>
Full article ">Figure 4
<p>2D FEM model of the gravity dam section.</p>
Full article ">Figure 5
<p>Positions of the measurement points in the gravity dam section.</p>
Full article ">Figure 6
<p>The deformation of the gravity dam under different water loads (unit: m).</p>
Full article ">Figure 7
<p>Results of deformation separation (<math display="inline"><semantics> <msub> <mi>h</mi> <mi>w</mi> </msub> </semantics></math> = 0.8 <math display="inline"><semantics> <msub> <mi>h</mi> <mi>d</mi> </msub> </semantics></math>, unit: m).</p>
Full article ">Figure 8
<p>Results of deformation separation (<math display="inline"><semantics> <msub> <mi>h</mi> <mi>w</mi> </msub> </semantics></math> = <math display="inline"><semantics> <msub> <mi>h</mi> <mi>d</mi> </msub> </semantics></math>, unit: m).</p>
Full article ">Figure 9
<p>FEM model of the arch dam.</p>
Full article ">Figure 10
<p>Layout of plumbs for the arch dam.</p>
Full article ">Figure 11
<p>Contour plot of downstream displacement distribution (unit: m).</p>
Full article ">Figure 12
<p>Contour plot of cross-stream displacement distribution (unit: m).</p>
Full article ">Figure 13
<p>Contour plot of vertical displacement distribution (unit: m).</p>
Full article ">Figure 14
<p>Layout of plumb for the arch dam, different colors represent different virtual springs.</p>
Full article ">Figure 15
<p>Distribution of measurement point errors (RE).</p>
Full article ">Figure 16
<p>RRMSE for different numbers of virtual springs.</p>
Full article ">Figure 17
<p>Dam material division diagram.</p>
Full article ">Figure 18
<p>Water level monitoring time history curve.</p>
Full article ">Figure 19
<p>Temperature monitoring time history curve.</p>
Full article ">Figure 20
<p>Displacements measured by some plumb lines.</p>
Full article ">Figure 21
<p>Optimisation process for the inversion of dam parameters.</p>
Full article ">
21 pages, 6033 KiB  
Article
SISGAN: A Generative Adversarial Network Pedestrian Trajectory Prediction Model Combining Interaction Information and Scene Information
by Wanqing Dou and Lili Lu
Appl. Sci. 2024, 14(20), 9537; https://doi.org/10.3390/app14209537 (registering DOI) - 18 Oct 2024
Abstract
Accurate pedestrian trajectory prediction is crucial in many fields. This requires the full use and learning of pedestrians’ social interactions, movements, and environmental information. In view of the current research on pedestrian trajectory prediction, wherein most of the pedestrian interaction information is explored [...] Read more.
Accurate pedestrian trajectory prediction is crucial in many fields. This requires the full use and learning of pedestrians’ social interactions, movements, and environmental information. In view of the current research on pedestrian trajectory prediction, wherein most of the pedestrian interaction information is explored from the level of overall interaction, this paper proposes the SISGAN model, which designs a social interaction module from the perspective of the target pedestrian, and takes four kinds of interaction information as the influencing factors of pedestrian interaction, so as to describe the influence mechanism of pedestrian–pedestrian interaction. In addition, in terms of environmental information, the index density of pedestrian historical trajectory in space is taken into account in the extraction of environmental information, which increases the potential correlation between environmental information and pedestrians. Finally, we integrate social interaction information and environmental information and make the final trajectory prediction based on GAN. Experiments on ETH and UCY datasets demonstrate the effectiveness of the SISGAN model proposed in this paper. Full article
(This article belongs to the Special Issue Advanced, Smart, and Sustainable Transportation)
24 pages, 6356 KiB  
Article
The Evaluation of Global and Regional Applications of Modeling Platform Across Scales-Atmosphere (MPAS) Against Weather Research Forecast (WRF) Model over California for a Winter (2013 DISCOVER-AQ) and Summer (2016 CABOTS) Episode
by Kemal Gürer, Zhan Zhao, Chenxia Cai and Jeremy C. Avise
Atmosphere 2024, 15(10), 1248; https://doi.org/10.3390/atmos15101248 (registering DOI) - 18 Oct 2024
Abstract
The Modeling Platform Across Scales-Atmosphere (MPAS) was used to simulate meteorological conditions for a two-week winter episode during 10–23 January 2013, and a two-week summer episode during 18–31 July 2016, using both as a global model and a regional model with a focus [...] Read more.
The Modeling Platform Across Scales-Atmosphere (MPAS) was used to simulate meteorological conditions for a two-week winter episode during 10–23 January 2013, and a two-week summer episode during 18–31 July 2016, using both as a global model and a regional model with a focus on California. The results of both global and regional applications of MPAS were compared against the surface and upper air rawinsonde observations while the variations of characteristic meteorological variables and modeling errors were evaluated in space, time, and statistical sense. The results of the Advanced Weather Research and Forecast (WRF-ARW, hereafter WRF) model simulations for the same episodes were also used to evaluate the results of both applications of MPAS. The temporal analyses performed at surface stations indicate that both global and regional applications of MPAS and WRF model predict the diurnal evolution of characteristic meteorological parameters reasonably well in both winter and summer episodes studied here. The average diurnal bias in predicting 2 m temperature by MPAS and WRF are about the same with a maximum of 2 °C in winter and 1 °C in summer while that of 2 m mixing ratio is within 1 g/kg for all three modeling applications. The rawinsonde profiles of temperature, dew point temperature, and wind direction agree reasonably well with observations while wind speed is underestimated by all three applications. The comparisons of the spatial distribution of anomaly correlation and mean bias errors calculated from each model results for 2 m temperature, 2 m water vapor mixing ratio, 10 m wind speed and wind direction indicate that all three models have similar magnitudes of agreement with observations as well as errors away from observations throughout California. Full article
(This article belongs to the Section Atmospheric Techniques, Instruments, and Modeling)
Show Figures

Figure 1

Figure 1
<p>The locations of 161 surface meteorological stations (black dots), 3 rawinsonde stations (orange dots, red labels; Oakland, Vandenberg AFB and Edwards AFB), along with 6 surface stations (black dots, red labels; Oakland, Sacramento, Fresno, Bakersfield, Los Angeles, and San Bernardino that were used to show temporal model evaluations in the manuscript) placed over the terrain relief map over California and neighboring states, Oregon (OR), Idaho (ID), Utah (UT), Arizona (AZ), and country of Mexico (MEX) (black capital letters). Sacramento Valley (SV) and San Joaquin Valley (SJV) are also shown with elevated terrain that surrounds them, namely Coastal Ranges and the Sierra Nevada Mountains (all were highlighted with blue text).</p>
Full article ">Figure 2
<p>Global MPAS modeling domain setup using varying resolution ranging from 3 to 48 km, where 3 km covers the states of California and Nevada (see <a href="#app1-atmosphere-15-01248" class="html-app">Figure S2</a> for the area of focus, or the evaluation domain used in this study).</p>
Full article ">Figure 3
<p>Horizontal spatial distribution of (<b>a</b>) 10 m wind vectors, (<b>b</b>) 2 m temperature, and (<b>c</b>) 2 m relative humidity fields that are temporally averaged at 8 AM for the winter 2013 episode from WRF (<b>left</b>), global MPAS (<b>middle</b>) and regional MPAS (<b>right</b>) results.</p>
Full article ">Figure 4
<p>Temporal evolution of 2 m temperature, 2 m mixing ratio, 2 m relative humidity, and 10 m wind speed and direction predicted by global MPAS (blue), regional MPAS (red), and WRF (green) against the observations (black) at Bakersfield during 10–24 January 2013, episode.</p>
Full article ">Figure 5
<p>Diurnal evolution of (<b>a</b>) mean bias (BIAS), (<b>b</b>) mean absolute error (MAE), and (<b>c</b>) mean standard deviation (SDEV) of 2 m temperature, and diurnal evolution of (<b>d</b>) mean bias (BIAS), (<b>e</b>) mean absolute error (MAE), and (<b>f</b>) mean standard deviation (SDEV) of 2 m mixing ratio that are averaged over the California evaluation domain for 2013 winter episode.</p>
Full article ">Figure 6
<p>Rawinsonde observations (<b>upper left</b>) and model predictions of global MPAS (<b>upper right</b>), regional MPAS (<b>lower right</b>) and WRF (<b>lower left</b>) on 15 January 2013, 00Z at Oakland, CA are given in skew-T/log-P diagram. Black line is the observed temperature, blue line is the dew point temperature, and wind barbs on the right show the wind speed and direction with height.</p>
Full article ">Figure 7
<p>Horizontal spatial distribution of (<b>a</b>) 10 m wind vectors, (<b>b</b>) 2 m temperature, and (<b>c</b>) 2 m relative humidity that are temporally averaged at 8 AM during the summer 2016 episode from WRF (<b>left</b>), global MPAS (<b>middle</b>) and regional MPAS (<b>right</b>) results.</p>
Full article ">Figure 7 Cont.
<p>Horizontal spatial distribution of (<b>a</b>) 10 m wind vectors, (<b>b</b>) 2 m temperature, and (<b>c</b>) 2 m relative humidity that are temporally averaged at 8 AM during the summer 2016 episode from WRF (<b>left</b>), global MPAS (<b>middle</b>) and regional MPAS (<b>right</b>) results.</p>
Full article ">Figure 8
<p>Temporal evolution of 2 m temperature, 2 m mixing ratio, 2 m relative humidity, 10 m wind speed and direction at Bakersfield, CA during 18–31 July 2016 episode, as estimated by global MPAS (blue), regional MPAS (red) and WRF (green) against observations (black).</p>
Full article ">Figure 9
<p>Diurnal evolution of bias (BIAS), mean absolute error (MAE) and standard deviation (SDEV) of 2 m temperature (<b>a</b>–<b>c</b>) and 2 m mixing ratio (<b>d</b>–<b>f</b>) that are averaged over the evaluation domain for 2016 summer episode.</p>
Full article ">Figure 10
<p>Rawinsonde observations (<b>upper left</b>) and model predictions of global MPAS (<b>upper right</b>), regional MPAS (<b>lower right</b>) and WRF (<b>lower left</b>) on 20 July 2016, 12Z at Oakland, CA are given in skew-T/log-P diagram. Black line is the observed temperature, blue line is the dew point temperature, and wind barbs on the right show the wind speed and direction with height.</p>
Full article ">
Back to TopTop