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22 pages, 33216 KiB  
Article
Characterizing Sparse Spectral Diversity Within a Homogenous Background: Hydrocarbon Production Infrastructure in Arctic Tundra near Prudhoe Bay, Alaska
by Daniel Sousa, Latha Baskaran, Kimberley Miner and Elizabeth Josephine Bushnell
Remote Sens. 2025, 17(2), 244; https://doi.org/10.3390/rs17020244 - 11 Jan 2025
Viewed by 627
Abstract
We explore a new approach for the parsimonious, generalizable, efficient, and potentially automatable characterization of spectral diversity of sparse targets in spectroscopic imagery. The approach focuses on pixels which are not well modeled by linear subpixel mixing of the Substrate, Vegetation and Dark [...] Read more.
We explore a new approach for the parsimonious, generalizable, efficient, and potentially automatable characterization of spectral diversity of sparse targets in spectroscopic imagery. The approach focuses on pixels which are not well modeled by linear subpixel mixing of the Substrate, Vegetation and Dark (S, V, and D) endmember spectra which dominate spectral variance for most of Earth’s land surface. We illustrate the approach using AVIRIS-3 imagery of anthropogenic surfaces (primarily hydrocarbon extraction infrastructure) embedded in a background of Arctic tundra near Prudhoe Bay, Alaska. Computational experiments further explore sensitivity to spatial and spectral resolution. Analysis involves two stages: first, computing the mixture residual of a generalized linear spectral mixture model; and second, nonlinear dimensionality reduction via manifold learning. Anthropogenic targets and lakeshore sediments are successfully isolated from the Arctic tundra background. Dependence on spatial resolution is observed, with substantial degradation of manifold topology as images are blurred from 5 m native ground sampling distance to simulated 30 m ground projected instantaneous field of view of a hypothetical spaceborne sensor. Degrading spectral resolution to mimicking the Sentinel-2A MultiSpectral Imager (MSI) also results in loss of information but is less severe than spatial blurring. These results inform spectroscopic characterization of sparse targets using spectroscopic images of varying spatial and spectral resolution. Full article
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<p>Location. The Brooks Range runs over 1000 km from the Chukchi Sea, across northern Alaska, into the Yukon Territory. Its north slope, running to the Arctic Ocean, hosts the Prudhoe Bay Oil Field. Discovered on 12 March 1968 by ARCO and Exxon, Prudhoe Bay field is commonly recognized as the largest in North America. Estimates of original oil volume are 25 billion barrels. Production at Prudhoe Bay came onstream in the late 1970s and continues to present.</p>
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<p>AVIRIS-3 flight line overview. The first component of the analysis uses an example flight line (AV320230806t205810) acquired on 6 August 2023. These data were collected at approximately 4100 m (13,450 ft) flying in a north–south orientation. True color (<b>left</b>) and false color (<b>right</b>) images show Level-2A ISOFIT-corrected reflectance in north up orientation. A linear 2% stretch is applied to both images. Ground sampling distance is 4.1 m. Hydrocarbon extraction infrastructure is clearly visible amongst a typical north slope landscape mosaic of permafrost and thermokarst lakes. Yellow squares show the three 400 × 400 pixel subsets mosaiced and used for subsequent analysis.</p>
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<p>Principal Component based spectral feature space of the AVIRIS-3 dataset. The natural permafrost + thermokarst background forms a mixing space between Dark (D), green vegetation (V), and nonphotosynthetic vegetation (N) endmembers. This mixing continuum dominates image variance. Anthropogenic substrates (S<sub>1</sub>–S<sub>6</sub>) and processes, like Flaring (F), are spatially sparse but spectrally highly distinct, forming excursions from the mixing space. Some human materials are characterized by consistent absorption features, like the SWIR absorption at 2.2 microns and longer wavelengths characteristic of many polymers. Anthropogenic materials are prominent in the PC transform, but full characterization is made challenging by depth of the embedding space (many PCs to explore) and redundancy (same spectra identified by multiple pairs of PC dimensions). Here we show examples through PC5, but no obvious stopping point is evident.</p>
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<p>2D UMAP spectral feature space of AVIRIS-3 reflectance. Additional Dark endmembers (D<sub>1</sub>–D<sub>3</sub>) are readily identified using UMAP but not using PCs 1 through 5 since their contribution to overall image variance is small. Mixing continua (e.g., from D<sub>2</sub> to V and N) endmembers are also clearly visible. The full complexity of the anthropogenic substrates (S) collapses onto a single submanifold which can be easily identified and isolated for targeted analysis. The primary UMAP hyperparameter, the number of Nearest Neighbors (NN), has a clear impact on manifold structure. Low values of NN (<b>left</b>) result in identification of a very large number of internally consistent but globally incoherent clusters which are effectively fitting to sensor/atmospheric correction noise. High values of NN (<b>right</b>) capture global manifold topology but can lose important low-variance details. An intermediate value (<b>center</b>) was selected for subsequent work. Spectra for D<sub>1</sub> and D<sub>3</sub> are shown on <a href="#remotesensing-17-00244-f005" class="html-fig">Figure 5</a>.</p>
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<p>3D UMAP feature space of AVIRIS-3 reflectance. Complexity is even more evident in the shallow water (Dark 1–3, or D<sub>1</sub>–D<sub>3</sub>) endmembers in the 3D embedding than the 2D embedding. Nonphotosynthetic vegetation (N), green vegetation (V) and anthropogenic substrate (S) EMs are present, but less clearly identifiable. Inspection of the embedding image (<a href="#remotesensing-17-00244-f006" class="html-fig">Figure 6</a>) shows that the UMAP clusters are capturing spatially coherent features.</p>
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<p>2D UMAP feature space of AVIRIS-3 spectral mixture residual. After removing the underlying mixing continuum, anthropogenic surfaces and processes are cleanly separable from the rest of the image (red polygon on feature space, red region of interest on image mosaic). Base image is a true color composite. A broad diversity of spectra (<b>lower left</b>) are contained within the statistically separable submanifold, corresponding to a wide range of infrastructure, including roads, pipelines, and extraction facilities. Some natural littoral features are also captured.</p>
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<p>Spectral diversity within the anthropogenic pixels identified from the UMAP(MR) space as shown by both PCs (<b>left</b>) and targeted UMAP (<b>right</b>). Spaces are sparser because most of the image is now excluded. UMAP clearly shows the albedo continuum, culminating in multiple tendrils near the bottom of the space, each of which corresponds to a distinct reflectance spectrum. Mixed pixels are clearly identifiable from each edge of the manifold. In contrast, the PC space manifests as a spiky hyperball, with individual mixing lines emanating from the body of the point cloud. In some cases, by not requiring statistical connectivity, the PCs are better able to identify compositional gradients among small numbers of pixels.</p>
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<p>Effect of spatial resolution on the characterization approach. Here we convolve the 4.1 m AVIRIS-3 reflectance mosaic with a low pass Gaussian blurring kernel to simulate the point spread function of a hypothetical 30 m resolution spaceborne imaging spectrometer. The resulting feature spaces are obviously much sparser. Broad spectral gradients corresponding to land cover types are evident, but clearly insufficient pixel density is present for either dimensionality reduction approach to resolve many important individual materials. Letter labels refer to the same endmember materials as <a href="#remotesensing-17-00244-f003" class="html-fig">Figure 3</a>, <a href="#remotesensing-17-00244-f004" class="html-fig">Figure 4</a> and <a href="#remotesensing-17-00244-f005" class="html-fig">Figure 5</a>.</p>
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<p>Effect of spectral resolution on the characterization approach. Here we convolve the AVIRIS-3 reflectance mosaic with the spectral response function of the Sentinel-2A multispectral imager to simulate the effect of spectral resolution, while holding spatial resolution constant. Shallow water still dominates the UMAP manifold structure. Anthropogenic materials still form an appreciable submanifold, but it is not fully separable from the main manifold even after pretreatment with the spectral mixture residual. Interested readers may benefit from comparison to Figure 6 of [<a href="#B17-remotesensing-17-00244" class="html-bibr">17</a>]. Letter labels refer to the same endmember materials as <a href="#remotesensing-17-00244-f003" class="html-fig">Figure 3</a>, <a href="#remotesensing-17-00244-f004" class="html-fig">Figure 4</a> and <a href="#remotesensing-17-00244-f005" class="html-fig">Figure 5</a>.</p>
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<p>Map view of key results. <b>Top row</b> shows true color (<b>left</b>) and false color (<b>right</b>) reflectance. <b>Middle row</b> shows true color (<b>left</b>) and false color (<b>right</b>) spectral mixture residual images. <b>Bottom row</b> shows dimensionality reduction results from UMAP dimensions (<b>left</b>) and PCs (<b>right</b>).</p>
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<p>Sensitivity of 3D covariance-based Principal Component spectral feature space of AVIRIS-3 reflectance to coarsening spatial resolution. The body of the point cloud is compressed towards the corner of the scatterplots to accommodate the wide range of spatially sparse high-variance pixels associated with emission spectra from methane flaring and spurious BRDF effects. A clear step change occurs between 16 and 32 m resolution, surprisingly consistent with [<a href="#B61-remotesensing-17-00244" class="html-bibr">61</a>].</p>
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<p>Sensitivity of 2D UMAP spectral feature space of AVIRIS-3 reflectance to coarsening spatial resolution. Manifold connectivity is greatest with fine spatial resolution (<b>above</b>) and degrades as resolution coarsens (<b>below</b>). For this dataset, 8 m resolution data (<b>top row</b>) captures similar manifold topology to the full 4 m resolution reflectance data (compare to <a href="#remotesensing-17-00244-f004" class="html-fig">Figure 4</a>), while 64 m resolution data (<b>bottom row</b>) retains only the most generic manifold properties.</p>
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<p>Sensitivity of 3D covariance-based Principal Component spectral feature space of AVIRIS-3 mixture residual reflectance to coarsening spatial resolution. The body of the point cloud is compressed towards the corner of the scatterplots to accommodate the wide range of spatially sparse high-variance pixels associated with emission spectra from methane flaring and spurious BRDF effects. As with <a href="#remotesensing-17-00244-f0A3" class="html-fig">Figure A3</a>, a clear step change occurs between 16 and 32 m resolution.</p>
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<p>Sensitivity of 2D UMAP spectral feature space of AVIRIS-3 mixture residual reflectance to coarsening spatial resolution. As with UMAP (Reflectance), manifold connectivity is greatest with fine spatial resolution (<b>above</b>) and degrades as resolution coarsens (<b>below</b>).</p>
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31 pages, 2255 KiB  
Article
Information Geometry and Manifold Learning: A Novel Framework for Analyzing Alzheimer’s Disease MRI Data
by Ömer Akgüller, Mehmet Ali Balcı and Gabriela Cioca
Diagnostics 2025, 15(2), 153; https://doi.org/10.3390/diagnostics15020153 - 10 Jan 2025
Viewed by 317
Abstract
Background: Alzheimer’s disease is a progressive neurological condition marked by a decline in cognitive abilities. Early diagnosis is crucial but challenging due to overlapping symptoms among impairment stages, necessitating non-invasive, reliable diagnostic tools. Methods: We applied information geometry and manifold learning [...] Read more.
Background: Alzheimer’s disease is a progressive neurological condition marked by a decline in cognitive abilities. Early diagnosis is crucial but challenging due to overlapping symptoms among impairment stages, necessitating non-invasive, reliable diagnostic tools. Methods: We applied information geometry and manifold learning to analyze grayscale MRI scans classified into No Impairment, Very Mild, Mild, and Moderate Impairment. Preprocessed images were reduced via Principal Component Analysis (retaining 95% variance) and converted into statistical manifolds using estimated mean vectors and covariance matrices. Geodesic distances, computed with the Fisher Information metric, quantified class differences. Graph Neural Networks, including Graph Convolutional Networks (GCN), Graph Attention Networks (GAT), and GraphSAGE, were utilized to categorize impairment levels using graph-based representations of the MRI data. Results: Significant differences in covariance structures were observed, with increased variability and stronger feature correlations at higher impairment levels. Geodesic distances between No Impairment and Mild Impairment (58.68, p<0.001) and between Mild and Moderate Impairment (58.28, p<0.001) are statistically significant. GCN and GraphSAGE achieve perfect classification accuracy (precision, recall, F1-Score: 1.0), correctly identifying all instances across classes. GAT attains an overall accuracy of 59.61%, with variable performance across classes. Conclusions: Integrating information geometry, manifold learning, and GNNs effectively differentiates AD impairment stages from MRI data. The strong performance of GCN and GraphSAGE indicates their potential to assist clinicians in the early identification and tracking of Alzheimer’s disease progression. Full article
(This article belongs to the Special Issue Artificial Intelligence in Alzheimer’s Disease Diagnosis)
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<p>Covariance matrices for impairment classes.</p>
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<p>Geodesic distance matrix heat map between impairment classes.</p>
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<p>Intra-class variability across impairment classes.</p>
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<p>PGA - Explained variables.</p>
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<p>UMAP visualization of impairment classes.</p>
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<p>Comparative analysis of GCN, GAT, and GraphSAGE in classification using information-theoretic geodesic graph representations.</p>
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<p>Confusion matrices of GCN, GAT, and GraphSAGE in the classification of different impairment classes.</p>
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20 pages, 305 KiB  
Article
Derivation of Tensor Algebra as a Fundamental Operation—The Fermi Derivative in a General Metric Affine Space
by Michael Tsamparlis
Symmetry 2025, 17(1), 81; https://doi.org/10.3390/sym17010081 - 7 Jan 2025
Viewed by 323
Abstract
The aim of this work is to demonstrate that all linear derivatives of the tensor algebra over a smooth manifold M can be viewed as specific cases of a broader concept—the operation of derivation. This approach reveals the universal role of differentiation, which [...] Read more.
The aim of this work is to demonstrate that all linear derivatives of the tensor algebra over a smooth manifold M can be viewed as specific cases of a broader concept—the operation of derivation. This approach reveals the universal role of differentiation, which simplifies and generalizes the study of tensor derivatives, making it a powerful tool in Differential Geometry and related fields. To perform this, the generic derivative is introduced, which is defined in terms of the quantities Qk(i)(X). Subsequently, the transformation law of these quantities is determined by the requirement that the generic derivative of a tensor is a tensor. The quantities Qk(i)(X) and their transformation law define a specific geometric object on M, and consequently, a geometric structure on M. Using the generic derivative, one defines the tensor fields of torsion and curvature and computes them for all linear derivatives in terms of the quantities Qk(i)(X). The general model is applied to the cases of Lie derivative, covariant derivative, and Fermi derivative. It is shown that the Lie derivative has non-zero torsion and zero curvature due to the Jacobi identity. For the covariant derivative, the standard results follow without any further calculations. Concerning the Fermi derivative, this is defined in a new way, i.e., as a higher-order derivative defined in terms of two derivatives: a given derivative and the Lie derivative. Being linear derivative, it has torsion and curvature tensor. These fields are computed in a general affine space from the corresponding general expressions of the generic derivative. Applications of the above considerations are discussed in a number of cases. Concerning the Lie derivative, it is been shown that the Poisson bracket is in fact a Lie derivative. Concerning the Fermi derivative, two applications are considered: (a) the explicit computation of the Fermi derivative in a general affine space and (b) the consideration of Freedman–Robertson–Walker spacetime endowed with a scalar torsion field, which satisfies the Cosmological Principle and the computation of Fermi derivative of the spatial directions defining a spatial frame along the cosmological fluid of comoving observers. It is found that torsion, even in this highly symmetric case, induces a kinematic rotation of the space axes, questioning the interpretation of torsion as a spin. Finally it is shown that the Lie derivative of the dynamical equations of an autonomous conservative dynamical system is equivalent to the standard Lie symmetry method. Full article
(This article belongs to the Special Issue Advances in Nonlinear Systems and Symmetry/Asymmetry)
17 pages, 1240 KiB  
Technical Note
MAL-Net: Model-Adaptive Learned Network for Slow-Time Ambiguity Function Shaping
by Jun Wang, Xiangqing Xiao, Jinfeng Hu, Ziwei Zhao, Kai Zhong and Chaohai Li
Remote Sens. 2025, 17(1), 173; https://doi.org/10.3390/rs17010173 - 6 Jan 2025
Viewed by 333
Abstract
Designing waveforms with a Constant Modulus Constraint (CMC) to achieve desirable Slow-Time Ambiguity Function (STAF) characteristics is significantly important in radar technology. The problem is NP-hard, due to its non-convex quartic objective function and CMC constraint. Existing methods typically involve model-based approaches with [...] Read more.
Designing waveforms with a Constant Modulus Constraint (CMC) to achieve desirable Slow-Time Ambiguity Function (STAF) characteristics is significantly important in radar technology. The problem is NP-hard, due to its non-convex quartic objective function and CMC constraint. Existing methods typically involve model-based approaches with relaxation and data-driven Deep Neural Networks (DNNs) methods, which face the challenge of dataimitation. We observe that the Complex Circle Manifold (CCM) naturally satisfies the CMC. By projecting onto the CCM, the problem is transformed into an unconstrained minimization problem that can be tackled using the CCM gradient descent model. Furthermore, we observe that the gradient descent model over the CCM can be unfolded as a Deep Learning (DL) network. Therefore, byeveraging the powerfulearning ability of DL and the CCM gradient descent model, we propose a Model-Adaptive Learned Network (MAL-Net) method without relaxation. Initially, we reformulate the problem as an Unconstrained Quartic Problem (UQP) on the CCM. Then, the MAL-Net is developed toearn the step sizes of allayers adaptively. This is accomplished by unrolling the CCM gradient descent model as the networkayer. Our simulation results demonstrate that the proposed MAL-Net achieves superior STAF performance compared to existing methods. Full article
(This article belongs to the Special Issue Advances in Remote Sensing, Radar Techniques, and Their Applications)
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<p>Gradient descent model over the CCM.</p>
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<p>The structure of the Model-Adaptive Learned Network (MAL-Net).</p>
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<p>Convergence performance of different networkayers.</p>
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<p>Comparisons of the nulling STAF: (<b>a</b>) UniAFSIM [<a href="#B20-remotesensing-17-00173" class="html-bibr">20</a>]; (<b>b</b>) QGD [<a href="#B21-remotesensing-17-00173" class="html-bibr">21</a>]; (<b>c</b>) MOEM [<a href="#B22-remotesensing-17-00173" class="html-bibr">22</a>]; (<b>d</b>) ResNet [<a href="#B25-remotesensing-17-00173" class="html-bibr">25</a>]; (<b>e</b>) proposed method.</p>
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<p>STAF with range cut at (<b>a</b>) <span class="html-italic">r</span> = 2, (<b>b</b>) <span class="html-italic">r</span> = 3, (<b>c</b>) <span class="html-italic">r</span> = 4.</p>
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<p>Range−velocity planes of the CAF for (<b>a</b>) non-optimized, (<b>b</b>) proposed method.</p>
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15 pages, 1013 KiB  
Article
Increasing IQ Test Scores and Decreasing g: The Flynn Effect and Decreasing Positive Manifold Strengths in Austria (2005–2018)
by Denise Andrzejewski, Sandra Oberleiter, Marco Vetter and Jakob Pietschnig
J. Intell. 2024, 12(12), 130; https://doi.org/10.3390/jintelligence12120130 - 23 Dec 2024
Viewed by 571
Abstract
After almost a century of global generational IQ test score gains, the Flynn effect has, in the past decades, been observed to show stagnation and reversals in several countries. Tentative evidence from academic achievement data has suggested that these trajectory changes may be [...] Read more.
After almost a century of global generational IQ test score gains, the Flynn effect has, in the past decades, been observed to show stagnation and reversals in several countries. Tentative evidence from academic achievement data has suggested that these trajectory changes may be rooted in a decreasing strength of the positive manifold of intelligence due to increasing ability differentiation and specialization in the general population. Here, we provide direct evidence for generational IQ test score and positive manifold strength changes based on IQ test standardization data from 1392 Austrian residents between 2005 and 2018. Our analyses revealed positive Flynn effects across all domains of the IQ test (Cohen’s d from 0.21 to 0.91) but a trend toward decreasing strength in the positive manifold of intelligence (R2 from .908 to .892), though these changes were not statistically significant. Our results are consistent with the idea that increasingly inconsistent Flynn effect trajectories may be attributed to increasing ability differentiation and specialization in the general population over time. Full article
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<p>R<sup>2</sup> values over time for the raw and latent scores.</p>
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19 pages, 7453 KiB  
Article
Velocity Observer Design for Tether Deployment in Hamiltonian Framework
by Jihang Yang, Guanzheng Chen, Mingming Zhang, Gangqiang Li and Jinyu Liu
Aerospace 2024, 11(12), 1047; https://doi.org/10.3390/aerospace11121047 - 20 Dec 2024
Viewed by 417
Abstract
This paper presents a nonlinear velocity observer of tether deployment using the immersion and invariance technique, and the velocity observer design problem is recast as a problem of designing an attractive and invariant manifold inside the Hamiltonian framework. The passivity-based control theory is [...] Read more.
This paper presents a nonlinear velocity observer of tether deployment using the immersion and invariance technique, and the velocity observer design problem is recast as a problem of designing an attractive and invariant manifold inside the Hamiltonian framework. The passivity-based control theory is used to define an expected Hamiltonian function, and the stability of the designed velocity observer is addressed by using the passivity-based methodology. Finally, a simple tension control law with measurable and unmeasurable states is employed for controlling the tether deployment, where the unmeasurable states use the proposed velocity observer. Numerical simulations demonstrate that the proposed velocity observer is working successfully. Sensitivity analyses are conducted to test the effectiveness and robustness of the proposed velocity observer. Full article
(This article belongs to the Special Issue Application of Tether Technology in Space)
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<p>Schematic diagram of the space tether system.</p>
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<p>Time histories of non-dimensional tether length, in-plane libration angle, and input tension.</p>
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<p>Time histories of the states: (<b>a</b>) <math display="inline"><semantics> <mover accent="true"> <mi>λ</mi> <mo>^</mo> </mover> </semantics></math> and (<b>b</b>) <math display="inline"><semantics> <mover accent="true"> <mi>θ</mi> <mo>^</mo> </mover> </semantics></math> of the observer dynamics.</p>
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<p>Time histories of the estimated velocities: (<b>a</b>) <math display="inline"><semantics> <mover accent="true"> <mover accent="true"> <mi>λ</mi> <mo>^</mo> </mover> <mo>˙</mo> </mover> </semantics></math> and (<b>b</b>) <math display="inline"><semantics> <mover accent="true"> <mover accent="true"> <mi>θ</mi> <mo>^</mo> </mover> <mo>˙</mo> </mover> </semantics></math>.</p>
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<p>Time histories of the estimated velocities: (<b>a</b>) <math display="inline"><semantics> <mover accent="true"> <mover accent="true"> <mi>λ</mi> <mo>^</mo> </mover> <mo>˙</mo> </mover> </semantics></math> and (<b>b</b>) <math display="inline"><semantics> <mover accent="true"> <mover accent="true"> <mi>θ</mi> <mo>^</mo> </mover> <mo>˙</mo> </mover> </semantics></math> (magnified).</p>
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<p>Time histories of the Velocity errors: (<b>a</b>) <math display="inline"><semantics> <mrow> <mover accent="true"> <mover accent="true"> <mi>λ</mi> <mo>^</mo> </mover> <mo>˙</mo> </mover> <mo>−</mo> <mover accent="true"> <mi>λ</mi> <mo>˙</mo> </mover> </mrow> </semantics></math> and (<b>b</b>) <math display="inline"><semantics> <mrow> <mover accent="true"> <mover accent="true"> <mi>θ</mi> <mo>^</mo> </mover> <mo>˙</mo> </mover> <mo>−</mo> <mover accent="true"> <mi>θ</mi> <mo>˙</mo> </mover> </mrow> </semantics></math>.</p>
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<p>Time histories of the scaling factor <span class="html-italic">r</span>.</p>
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<p>Time histories of real measurement states: (<b>a</b>) <math display="inline"><semantics> <mover accent="true"> <mover accent="true"> <mi>λ</mi> <mo>^</mo> </mover> <mo>˙</mo> </mover> </semantics></math> and (<b>b</b>) <math display="inline"><semantics> <mover accent="true"> <mover accent="true"> <mi>θ</mi> <mo>^</mo> </mover> <mo>˙</mo> </mover> </semantics></math> with noise model.</p>
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<p>Time histories of estimated velocity <math display="inline"><semantics> <mover accent="true"> <mover accent="true"> <mi>λ</mi> <mo>^</mo> </mover> <mo>˙</mo> </mover> </semantics></math> with different values of the velocity gain.</p>
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<p>Time histories of estimated velocity <math display="inline"><semantics> <mover accent="true"> <mover accent="true"> <mi>θ</mi> <mo>^</mo> </mover> <mo>˙</mo> </mover> </semantics></math> with different values of the velocity gain.</p>
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<p>Time histories of the estimated velocities: (<b>a</b>) <math display="inline"><semantics> <mover accent="true"> <mover accent="true"> <mi>λ</mi> <mo>^</mo> </mover> <mo>˙</mo> </mover> </semantics></math> and (<b>b</b>) <math display="inline"><semantics> <mover accent="true"> <mover accent="true"> <mi>θ</mi> <mo>^</mo> </mover> <mo>˙</mo> </mover> </semantics></math> with measurement noise when gain <math display="inline"><semantics> <mrow> <msub> <mi>k</mi> <mn>1</mn> </msub> <mo>=</mo> <mn>1.0</mn> </mrow> </semantics></math>.</p>
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<p>Time histories of the states: (<b>a</b>) <math display="inline"><semantics> <mover accent="true"> <mi>λ</mi> <mo>^</mo> </mover> </semantics></math> and (<b>b</b>) <math display="inline"><semantics> <mover accent="true"> <mi>θ</mi> <mo>^</mo> </mover> </semantics></math> of the observer dynamics at different initial velocities.</p>
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<p>Time histories of the estimated velocities (<b>a</b>) <math display="inline"><semantics> <mover accent="true"> <mover accent="true"> <mi>λ</mi> <mo>^</mo> </mover> <mo>˙</mo> </mover> </semantics></math> and (<b>b</b>) <math display="inline"><semantics> <mover accent="true"> <mover accent="true"> <mi>θ</mi> <mo>^</mo> </mover> <mo>˙</mo> </mover> </semantics></math> at different initial velocities.</p>
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<p>Time histories of the states (<b>a</b>) <math display="inline"><semantics> <mover accent="true"> <mi>λ</mi> <mo>^</mo> </mover> </semantics></math> and (<b>b</b>) <math display="inline"><semantics> <mover accent="true"> <mi>θ</mi> <mo>^</mo> </mover> </semantics></math> of the observer dynamics with angle rates at different initial velocities.</p>
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<p>Time histories of the estimated velocities: (<b>a</b>) <math display="inline"><semantics> <mover accent="true"> <mover accent="true"> <mi>λ</mi> <mo>^</mo> </mover> <mo>˙</mo> </mover> </semantics></math> and (<b>b</b>) <math display="inline"><semantics> <mover accent="true"> <mover accent="true"> <mi>θ</mi> <mo>^</mo> </mover> <mo>˙</mo> </mover> </semantics></math> with angle rates at different initial velocities.</p>
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19 pages, 2198 KiB  
Article
Observer Design for State and Parameter Estimation for Two-Time-Scale Nonlinear Systems
by Zhenyu Xiao and Zhaoyang Duan
Processes 2024, 12(12), 2875; https://doi.org/10.3390/pr12122875 - 16 Dec 2024
Viewed by 505
Abstract
The design and calculation of nonlinear observers for parameter estimation in multi-time-scale nonlinear systems present significant challenges due to the inherent complexity and stiffness of such systems. This study proposes a framework for designing observers for two-time-scale nonlinear systems, with the objective of [...] Read more.
The design and calculation of nonlinear observers for parameter estimation in multi-time-scale nonlinear systems present significant challenges due to the inherent complexity and stiffness of such systems. This study proposes a framework for designing observers for two-time-scale nonlinear systems, with the objective of overcoming the aforementioned challenges. The design procedure involves reducing the original two-time-scale nonlinear system to a lower-dimensional model that captures only the slow dynamics while approximating the fast states through the use of an algebraic slow motion invariant manifold function. Subsequently, an exponential observer can be devised for this reduced system, which is valid for both state and parameter estimation. By employing the output from the original system, this observer can be adapted for online state and parameter estimation for the detailed two-time-scale system. The challenges associated with estimating parameters in two-time-scale nonlinear systems, the complexities of designing observers for such systems, and the computational burden associated with computing observers for ill-conditioned systems can be effectively addressed through the application of this design framework. A rigorous error analysis validates the convergence of the proposed observer towards the states and parameters of the original system. The viability and necessity of this observer design framework are demonstrated through a numerical example and an anaerobic digestion process. This study presents a practical approach for state and parameter estimation with observers for two-time-scale nonlinear systems. Full article
(This article belongs to the Special Issue Sustainable Chemical Engineering Processes and Intensification)
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<p>Observer design methodology.</p>
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<p>Dynamic response for actual and estimated states and parameter of the numerical system. (<b>a</b>) Actual and estimated values of <math display="inline"><semantics> <mrow> <msub> <mi>x</mi> <mn>1</mn> </msub> </mrow> </semantics></math>; (<b>b</b>) Actual and estimated values of <math display="inline"><semantics> <mrow> <msub> <mi>x</mi> <mn>2</mn> </msub> </mrow> </semantics></math>; (<b>c</b>) Actual and estimated values of <math display="inline"><semantics> <mrow> <msub> <mi>x</mi> <mn>3</mn> </msub> </mrow> </semantics></math>; (<b>d</b>) Actual and estimated values of <math display="inline"><semantics> <mrow> <msub> <mi>p</mi> <mn>1</mn> </msub> </mrow> </semantics></math>.</p>
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<p>Estimation errors for states and parameters of the numerical system. (<b>a</b>) Estimation error of <math display="inline"><semantics> <mrow> <msub> <mi>x</mi> <mn>1</mn> </msub> </mrow> </semantics></math>; (<b>b</b>) Estimation error of <math display="inline"><semantics> <mrow> <msub> <mi>x</mi> <mn>2</mn> </msub> </mrow> </semantics></math>; (<b>c</b>) Estimation error of <math display="inline"><semantics> <mrow> <msub> <mi>x</mi> <mn>3</mn> </msub> </mrow> </semantics></math>; (<b>d</b>) Estimation error of <math display="inline"><semantics> <mrow> <msub> <mi>p</mi> <mn>1</mn> </msub> </mrow> </semantics></math>.</p>
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<p>Comparison of original system values and estimated values for states and parameter (<b>a</b>) Actual and estimated values of <math display="inline"><semantics> <mrow> <msub> <mi>X</mi> <mn>1</mn> </msub> </mrow> </semantics></math>; (<b>b</b>) Actual and estimated values of <math display="inline"><semantics> <mrow> <msub> <mi>S</mi> <mn>1</mn> </msub> </mrow> </semantics></math>; (<b>c</b>) Actual and estimated values of <math display="inline"><semantics> <mrow> <msub> <mi>X</mi> <mn>2</mn> </msub> </mrow> </semantics></math>; (<b>d</b>) Actual and estimated values of <math display="inline"><semantics> <mrow> <msub> <mi>S</mi> <mn>2</mn> </msub> </mrow> </semantics></math>; (<b>e</b>) Actual and estimated values of <math display="inline"><semantics> <mrow> <msub> <mi>Y</mi> <mn>2</mn> </msub> </mrow> </semantics></math>.</p>
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<p>Observer estimation error of the anaerobic digestion system (the concentration of <math display="inline"><semantics> <mrow> <msub> <mi>X</mi> <mn>1</mn> </msub> </mrow> </semantics></math>, <math display="inline"><semantics> <mrow> <msub> <mi>X</mi> <mn>2</mn> </msub> </mrow> </semantics></math>, <math display="inline"><semantics> <mrow> <msub> <mi>S</mi> <mn>1</mn> </msub> </mrow> </semantics></math>, <math display="inline"><semantics> <mrow> <msub> <mi>S</mi> <mn>2</mn> </msub> </mrow> </semantics></math> are in g/L and the concentration of <math display="inline"><semantics> <mrow> <msub> <mi>Y</mi> <mn>2</mn> </msub> </mrow> </semantics></math> is in g/g).</p>
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10 pages, 243 KiB  
Article
Disaffinity Vectors on a Riemannian Manifold and Their Applications
by Sharief Deshmukh, Amira Ishan and Bang-Yen Chen
Mathematics 2024, 12(23), 3659; https://doi.org/10.3390/math12233659 - 22 Nov 2024
Cited by 1 | Viewed by 504
Abstract
A disaffinity vector on a Riemannian manifold (M,g) is a vector field whose affinity tensor vanishes. In this paper, we observe that nontrivial disaffinity functions offer obstruction to the topology of M and show that the existence of a [...] Read more.
A disaffinity vector on a Riemannian manifold (M,g) is a vector field whose affinity tensor vanishes. In this paper, we observe that nontrivial disaffinity functions offer obstruction to the topology of M and show that the existence of a nontrivial disaffinity function on M does not allow M to be compact. A characterization of the Euclidean space is also obtained by using nontrivial disaffinity functions. Further, we study properties of disaffinity vectors on M and prove that every Killing vector field is a disaffinity vector. Then, we prove that if the potential field ζ of a Ricci soliton M,g,ζ,λ is a disaffinity vector, then the scalar curvature is constant. As an application, we obtain conditions under which a Ricci soliton M,g,ζ,λ is trivial. Finally, we prove that a Yamabe soliton M,g,ξ,λ with a disaffinity potential field ξ is trivial. Full article
23 pages, 14187 KiB  
Article
Numerical Investigation of Combustion and Emission Characteristics of the Single-Cylinder Diesel Engine Fueled with Diesel-Ammonia Mixture
by Ali and Ocktaeck Lim
Energies 2024, 17(22), 5782; https://doi.org/10.3390/en17225782 - 19 Nov 2024
Viewed by 873
Abstract
This study proposes a dual-fuel approach combining diesel and ammonia in a single-cylinder compression ignition engine to reduce harmful emissions from internal combustion. Diesel is directly injected into the combustion chamber, while ammonia is introduced through the intake manifold with intake air. In [...] Read more.
This study proposes a dual-fuel approach combining diesel and ammonia in a single-cylinder compression ignition engine to reduce harmful emissions from internal combustion. Diesel is directly injected into the combustion chamber, while ammonia is introduced through the intake manifold with intake air. In this study, injection timing and the percentage of ammonia energy fraction was varied. A computational fluid dynamics (CFD) model simulates the combustion and emission processes to assess the impact of varying diesel injection timings and ammonia energy contributions. Findings indicate that as ammonia content increases, the engine experiences reductions in peak in-cylinder pressure, temperature, heat release rate, as well as overall efficiency and power output. Emission results suggest that greater ammonia usage leads to a reduction in soot, carbon monoxide, carbon dioxide, and unburned hydrocarbons, though a slight increase in nitrogen oxides emissions is observed. This analysis supports ammonia’s potential as a low-emission alternative fuel in future compression ignition engines. Full article
(This article belongs to the Topic Advanced Engines Technologies)
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<p>Schematic of the engine experimental setup.</p>
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<p>The experimental physical system.</p>
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<p>3D simulation model.</p>
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<p>Grid independency of simulation model.</p>
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<p>Research flow chart.</p>
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<p>Simulation model validation.</p>
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<p>In-cylinder pressure for various fuel concentration and SOI.</p>
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<p>Temperature for various fuel concentration and SOI.</p>
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<p>Temperature distribution of D100 and D50A50 with SOI: 20 BTDC, slice z axis position −0.003 m.</p>
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<p>Heat release rate for various fuel concentration and SOI.</p>
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<p>Peak of pressure rise rate.</p>
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<p>Combustion phasing.</p>
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<p>CA10, CA50 and CA90.</p>
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<p>10–90% burn duration.</p>
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<p>Ignition delay.</p>
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<p>IMEP.</p>
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<p>Indicated thermal efficiency.</p>
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<p>Combustion efficiency.</p>
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<p>Emissions produced from cases of combustion.</p>
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<p>NO<sub>x</sub> emission.</p>
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<p>CO and CO<sub>2</sub> percentage distribution of all species in D100 and D50A50 with SOI: 20 BTDC, slice z axis position −0.003 m.</p>
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<p>CO and CO<sub>2</sub> percentage distribution of all species in D100 and D50A50 with SOI: 20 BTDC, slice z axis position −0.003 m.</p>
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<p>NO<sub>x</sub> and Soot mass distribution of all species in D100 and D50A50 with SOI: 20 BTDC, slice z axis position −0.003 m.</p>
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18 pages, 6571 KiB  
Article
Influence of Solid Solution Treatment on Microstructure and Mechanical Properties of 20CrNiMo/Incoloy 825 Composite Materials
by Jie Liu, Qiang Li, Hailian Gui, Peng Zhang, Sha Li, Chen Zhang, Hao Liu, Chunlei Shen and Pengyue Zhang
Materials 2024, 17(22), 5588; https://doi.org/10.3390/ma17225588 - 15 Nov 2024
Viewed by 547
Abstract
The utilization of 20CrNiMo/Incoloy 825 composite materials as high-pressure pipe manifold steel can not only improve the strength and hardness of the steel, but also improve its corrosion resistance. However, research on the heat treatment of 20CrNiMo/Incoloy 825 composite materials is still scarce. [...] Read more.
The utilization of 20CrNiMo/Incoloy 825 composite materials as high-pressure pipe manifold steel can not only improve the strength and hardness of the steel, but also improve its corrosion resistance. However, research on the heat treatment of 20CrNiMo/Incoloy 825 composite materials is still scarce. Thus, the aim of this study was to investigate the influence of solid solution treatment on the microstructure and properties of 20CrNiMo/Incoloy 825 composite materials. Firstly, the composite materials were subjected to solid solution treatment at temperatures ranging from 850 to 1100 °C with varied holding times of 1 h, 4 h, and 6 h. Microstructural analysis revealed that the solid solution treatment temperature had a more pronounced effect than the treatment time on the interface decarburization layer, carburization layer, and grain size. It was observed that the carburized layer thickness decreased while the decarburized layer thickness increased with an increase in the solid solution treatment temperature, oil cooling was found to enhance the hardness of the base layer of the composite materials, and the size of the original austenite grains of 20CrNiMo steel and Incoloy 825 increased with an increase in the solid solution treatment temperature. Secondly, the tensile properties, microhardness, and fracture morphology were evaluated after the composite materials underwent solid solution treatment at temperatures between 950 °C and 1100 °C for 1 h. The results indicated that increasing the solution temperature initially led to an increase in tensile strength and elongation after fracture, followed by a decrease; furthermore, the hardness of Incoloy 825 exhibited a declining trend, while the hardness of 20CrNiMo first decreased then increased. Thirdly, the shear properties and interfacial element diffusion of the composite materials were analyzed following solid solution treatment in a temperature range of 950 °C to 1100 °C for 1 h. The findings demonstrated that higher solid solution treatment temperatures induced full diffusion of Cr, Ni, and Fe atoms at the interface and softened the matrix, leading to an increase in the thickness of the diffusion layer and toughening of the composite interface. Therefore, the shear strength increased with an increase in the solid solution treatment temperature. Finally, the optimal solid solution treatment process for 20CrNiMo/Incoloy 825 composite materials was determined to be 1050 °C/1 h oil cooling, following which the composite materials had good comprehensive mechanical properties. Full article
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<p>Specimen size: (<b>a</b>) tensile sample; (<b>b</b>) shear sample.</p>
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<p>Flow diagram of the experiment.</p>
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<p>Effect of solid solution treatment on the interface of 20CrNiMo/Incoloy 825 composite materials: (<b>a</b>) 850 °C/1 h oil cooling; (<b>b</b>) 850 °C/4 h oil cooling; (<b>c</b>) 850 °C/6 h air cooling; (<b>d</b>) 950 °C/1 h oil cooling; (<b>e</b>) 1050 °C/1 h oil cooling; (<b>f</b>) 1100 °C/1 h oil cooling.</p>
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<p>EBSD plots of 20CrNiMo/Incoloy 825 composite materials under different conditions.</p>
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<p>Map of 20CrNiMo steel after lath martensite transformation following solid solution treatment at 1050 °C/1 h: (<b>a</b>) IPF map; (<b>b</b>) original austenite grain distribution map; (<b>c</b>) martensite packet distribution map; (<b>d</b>) martensite variants distribution map; (<b>e</b>) the {001}, {011}, and {111} pole figures of martensite variant V24<sub>1</sub>; (<b>f</b>) the {001}, {011}, and {111} pole figures of martensite variant V24<sub>2</sub>; (<b>g</b>) the {001}, {011}, and {111} pole figures of martensite variant V6.</p>
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<p>Distribution maps of original austenite and residual austenite in steel 20CrNiMo under different solid solution treatment conditions: (<b>a</b>) 950 °C/1 h; (<b>b</b>) 1000 °C/1 h; (<b>c</b>) 1050 °C/1 h; (<b>d</b>) 1100 °C/1 h.</p>
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<p>Mechanical properties of 20CrNiMo/Incoloy 825 composite materials in different solid solution treatment processes: (<b>a</b>) the tensile stress–strain curve; (<b>b</b>) the tensile strength–temperature curve; (<b>c</b>) the elongation–temperature curve; (<b>d</b>) the hardness–temperature curve.</p>
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<p>The interfacial shear stress–displacement curves and shear strength of 20CrNiMo/Incoloy 825-clad plates with different solid solution treatment processes: (<b>a</b>) 950 °C/1 h; (<b>b</b>) 1000 °C/1 h; (<b>c</b>) 1050 °C/1 h; (<b>d</b>) 1100 °C/1 h; (<b>e</b>) EDS analysis at 1050 °C/1 h.</p>
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<p>The shear stress–displacement curves and shear strength of 20CrNiMo/Incoloy 825 composite materials with different solid solution treatment processes.</p>
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<p>EDS line scan at the interface of 20CrNiMo/Incoloy 825 composite material: (<b>a</b>) EDS line scan before solid solution treatment; (<b>b</b>) 950 °C; (<b>c</b>) 1000 °C; (<b>d</b>) 1050 °C; (<b>e</b>) 1100 °C.</p>
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<p>Experimental conclusion diagram. Ding [<a href="#B15-materials-17-05588" class="html-bibr">15</a>]; Liu et al. [<a href="#B17-materials-17-05588" class="html-bibr">17</a>]; Yu et al. [<a href="#B26-materials-17-05588" class="html-bibr">26</a>]; Ren et al. [<a href="#B27-materials-17-05588" class="html-bibr">27</a>]; Lim et al. [<a href="#B30-materials-17-05588" class="html-bibr">30</a>].</p>
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17 pages, 4885 KiB  
Article
An Experimental Investigation of the Effect of Two-Phase Flow in a Manifold on Water Jet Lengths
by Seyhmus Tumur, Arjin Ata and Tamer Bagatur
Water 2024, 16(22), 3263; https://doi.org/10.3390/w16223263 - 13 Nov 2024
Viewed by 612
Abstract
The outlet flow rates and changes in behaviors of five outlet ports where water and air–water (two-phase) mixtures pass horizontally in a manifold pipe system were investigated experimentally. The effects of different air-flow rates, vacuumed from the atmosphere with a Venturi device in [...] Read more.
The outlet flow rates and changes in behaviors of five outlet ports where water and air–water (two-phase) mixtures pass horizontally in a manifold pipe system were investigated experimentally. The effects of different air-flow rates, vacuumed from the atmosphere with a Venturi device in the system, on the outlet flow rates and diameters of the manifold port outlets were compared by measuring the outlet jet lengths. The system performance provided homogeneity of manifold port outlet flows and was tested. As a result, it was observed that homogeneous jet lengths were obtained in both single and two-phase low main manifold flows and equal outlet port diameters. When the main manifold flow rate V is 1.5–2 m/s, the system is stable and produces high jet lengths. The manifold pipe systems used in the experimental setup provide suitable working conditions for d/D = 0.433. The system does not show a smooth flow pattern with Venturi devices for d/D < 0.433. The low flow rates in this study’s tests are key. They are vital for designing micro irrigation systems. This depends on the critical d/D ratio of the system. Full article
(This article belongs to the Special Issue Advances in Hydraulic and Water Resources Research (2nd Edition))
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<p>Test setup (pump, water flow meter, air-flow meter, Venturi device, and manifold).</p>
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<p>Experimental setup with Venturi device.</p>
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<p>Experimental setup with Venturi deviceless device.</p>
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<p>Types of Venturi used in the experimental set.</p>
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<p>Manifold parameters (D = manifold main pipe diameter (1.27 cm), d = port outlet diameter (variable), L = manifold main pipe length (250 cm), and S= distance between ports (20 cm)).</p>
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<p>View of water jets issuing from the manifold and ports.</p>
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<p>Graph of comparison of water jet lengths in Venturi Type 1 Manifold Type 1 open, closed, and Venturi deviceless systems (<span class="html-italic">Q</span><sub>1</sub> = 17 × 10<sup>−5</sup> m<sup>3</sup>/s, <span class="html-italic">Q</span><sub>2</sub> = 20.8 × 10<sup>−5</sup> m<sup>3</sup>/s, <span class="html-italic">Q</span><sub>3</sub> = 23.6 × 10<sup>−5</sup> m<sup>3</sup>/s, <span class="html-italic">Q</span><sub>4</sub> = 27.8 × 10<sup>−5</sup> m<sup>3</sup>/s).</p>
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<p>Graph of comparison of water jet lengths in Venturi Type 1 Manifold Type 2 open, closed, and Venturi deviceless systems (<span class="html-italic">Q</span><sub>1</sub> = 17 × 10<sup>−5</sup> m<sup>3</sup>/s, <span class="html-italic">Q</span><sub>2</sub> = 20.8 × 10<sup>−5</sup> m<sup>3</sup>/s, <span class="html-italic">Q</span><sub>3</sub> = 23.6 × 10<sup>−5</sup> m<sup>3</sup>/s, <span class="html-italic">Q</span><sub>4</sub> = 27.8 × 10<sup>−5</sup> m<sup>3</sup>/s).</p>
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<p>Graph of comparison of water jet lengths in Venturi Type 1 Manifold Type 3 open, closed and Venturi deviceless systems (<span class="html-italic">Q</span><sub>1</sub> = 17 × 10<sup>−5</sup> m<sup>3</sup>/s, <span class="html-italic">Q</span><sub>2</sub> = 20.8 × 10<sup>−5</sup> m<sup>3</sup>/s, <span class="html-italic">Q</span><sub>3</sub> = 23.6 × 10<sup>−5</sup> m<sup>3</sup>/s, <span class="html-italic">Q</span><sub>4</sub> = 27.8 × 10<sup>−5</sup> m<sup>3</sup>/s).</p>
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<p>Graph of comparison of water jet lengths in Venturi Type 1 Manifold Type 4 open, closed, and Venturi deviceless systems (<span class="html-italic">Q</span><sub>1</sub> = 17 × 10<sup>−5</sup> m<sup>3</sup>/s, <span class="html-italic">Q</span><sub>2</sub> = 20.8 × 10<sup>−5</sup> m<sup>3</sup>/s, <span class="html-italic">Q</span><sub>3</sub> = 23.6 × 10<sup>−5</sup> m<sup>3</sup>/s, <span class="html-italic">Q</span><sub>4</sub> = 27.8 × 10<sup>−5</sup> m<sup>3</sup>/s).</p>
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<p>Graph of comparison of water jet lengths in Venturi Type 2 Manifold Type 1 open, closed, and Venturi deviceless systems (<span class="html-italic">Q</span><sub>1</sub> = 17 × 10<sup>−5</sup> m<sup>3</sup>/s, <span class="html-italic">Q</span><sub>2</sub> = 20.8 × 10<sup>−5</sup> m<sup>3</sup>/s, <span class="html-italic">Q</span><sub>3</sub> = 23.6 × 10<sup>−5</sup> m<sup>3</sup>/s, <span class="html-italic">Q</span><sub>4</sub> = 27.8 × 10<sup>−5</sup> m<sup>3</sup>/s).</p>
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<p>Graph of comparison of water jet lengths in Venturi Type 2 Manifold Type 2 open, closed, and Venturi deviceless systems (<span class="html-italic">Q</span><sub>1</sub> = 17 × 10<sup>−5</sup> m<sup>3</sup>/s, <span class="html-italic">Q</span><sub>2</sub> = 20.8 × 10<sup>−5</sup> m<sup>3</sup>/s, <span class="html-italic">Q</span><sub>3</sub> = 23.6 × 10<sup>−5</sup> m<sup>3</sup>/s, <span class="html-italic">Q</span><sub>4</sub> = 27.8 × 10<sup>−5</sup> m<sup>3</sup>/s).</p>
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<p>Graph of comparison of water jet lengths in Venturi Type 2 Manifold Type 3 open, closed and Venturi deviceless systems (<span class="html-italic">Q</span><sub>1</sub> = 17 × 10<sup>−5</sup> m<sup>3</sup>/s, <span class="html-italic">Q</span><sub>2</sub> = 20.8 × 10<sup>−5</sup> m<sup>3</sup>/s, <span class="html-italic">Q</span><sub>3</sub> = 23.6 × 10<sup>−5</sup> m<sup>3</sup>/s, <span class="html-italic">Q</span><sub>4</sub> = 27.8 × 10<sup>−5</sup> m<sup>3</sup>/s).</p>
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<p>Graph of comparison of water jet lengths in Venturi Type 2 Manifold Type 4 open, closed, and Venturi deviceless systems (<span class="html-italic">Q</span><sub>1</sub> = 17 × 10<sup>−5</sup> m<sup>3</sup>/s, <span class="html-italic">Q</span><sub>2</sub> = 20.8 × 10<sup>−5</sup> m<sup>3</sup>/s, <span class="html-italic">Q</span><sub>3</sub> = 23.6 × 10<sup>−5</sup> m<sup>3</sup>/s, <span class="html-italic">Q</span><sub>4</sub> = 27.8 × 10<sup>−5</sup> m<sup>3</sup>/s).</p>
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<p>D<sub>port</sub>/L<sub>jet</sub>−Q<sub>s</sub>/Q<sub>a</sub> scattering diagram in Venturi Type 1 experiment set.</p>
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<p>D<sub>port</sub>/L<sub>jet</sub>−Q<sub>s</sub>/Q<sub>a</sub> scattering diagram in Venturi Type 2 experiment set.</p>
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27 pages, 15970 KiB  
Article
The Influence of the Intake Geometry on the Performance of a Four-Stroke SI Engine for Aeronautical Applications
by Fabio Anaclerio, Annarita Viggiano, Francesco Fornarelli, Paolo Caso, Domenico Sparaco and Vinicio Magi
Energies 2024, 17(21), 5309; https://doi.org/10.3390/en17215309 - 25 Oct 2024
Viewed by 905
Abstract
In this work, the influence of plenum and port geometry on the performance of the intake process in a four-stroke spark ignition engine for ultralight aircraft applications is analyzed. Three intake systems are considered: the so-called “standard plenum”, with a relatively small plenum [...] Read more.
In this work, the influence of plenum and port geometry on the performance of the intake process in a four-stroke spark ignition engine for ultralight aircraft applications is analyzed. Three intake systems are considered: the so-called “standard plenum”, with a relatively small plenum volume, the “V1 plenum”, with a larger plenum volume, and the “standard plenum” equipped with a large curvature manifold called the “G2 port”. Both measurements and 3D CFD simulations, by using Ansys® Academic Fluent, Release 20.2, are performed to characterize and analyze the steady-flow field in the intake system for selected valve lifts. The experimental data and the numerical results are in excellent agreement with each other. The results show that at the maximum valve lift, i.e., 12 mm, the V1 plenum allows an increase in the air mass flow rate of 9.1% and 9.4% compared to the standard plenum and the standard plenum with the “G2 port”, respectively. In addition, the volumetric efficiency has been estimated under unsteady-flow conditions for all geometries at relatively high engine rpms. The difference between numerical results and measurements is less than 1% for the standard plenum, thus proving the accuracy of the model, which is then used to study the other configurations. The V1 plenum shows a fairly constant volumetric efficiency as the engine speed increases, although such an efficiency is lower than that of the other two geometries considered in this work. Specifically, the use of the “G2 port” leads to an increase of 1.5% in terms of volumetric efficiency with respect to the configuration with the original manifold. Furthermore, for the “G2 port” configuration, higher turbulent kinetic energy and higher swirl and tumble ratios are observed. This is expected to result in an improvement of air–fuel mixing and flame propagation. Full article
(This article belongs to the Special Issue Internal Combustion Engine Performance 2024)
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<p>Computer-aided design view of the 3D engine geometry: C1, C2, C3, and C4 stand for cylinder #1, cylinder #2, cylinder #3, and cylinder #4, respectively.</p>
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<p>Phase diagram of the engine working cycle.</p>
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<p>Exhaust and intake valve lifts as a function of CAD.</p>
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<p>Layout of the engine test bench. Black dashed lines refer to input signals for post-processing; red dashed lines refer to output signals for engine control; blue dashed lines refer to engine operating conditions.</p>
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<p>Layout of the SuperFlow SF-750 flow test bench. Pink arrows refer to flow air direction; red solid lines correspond to temperature signals; green solid lines refer to pressure signals; yellow line refers to blower speed control.</p>
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<p>Experimental and numerical pressure trace in the intake port for the standard plenum at 5000 rpm.</p>
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<p>Rendering of the three intake configurations: (<b>a</b>) baseline (standard plenum), (<b>b</b>) V1 plenum, and (<b>c</b>) standard plenum with G2 port.</p>
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<p>Rendering of the standard plenum (<b>a</b>) and V1 plenum (<b>b</b>).</p>
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<p>A detail of the baseline and V1 manifold (<b>a</b>) and G2 port (<b>b</b>).</p>
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<p>(<b>a</b>) Computational mesh for steady simulations. (<b>b</b>) Detail of the in-cylinder mesh along the intake valve axial plane.</p>
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<p>Computational mesh for unsteady simulations: (<b>a</b>) unstructured tetrahedral grid for plenum, intake manifold, cylinder #1, and exhaust duct; (<b>b</b>) a detail of cylinder #1 at 323 CAD.</p>
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<p>Dynamic remeshing of the computational grid on a crossing plane through the intake and exhaust valve axes (cylinder #1).</p>
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<p>Computational mesh for unsteady simulations: (<b>a</b>) coarse and (<b>b</b>) fine refinement.</p>
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<p>Intake volumetric flow rate as a function of valve lift.</p>
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<p>Streamlines and contour plots of velocity magnitude and velocity vectors on the intake valve axial plane with a valve lift of 12 mm: (<b>a</b>,<b>d</b>) baseline case; (<b>b</b>,<b>e</b>) V1 plenum; (<b>c</b>,<b>f</b>) standard plenum with G2 port.</p>
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<p>Front (<b>a</b>) and top (<b>b</b>) views of the half-way plane (red colored plane) with the curtain area (green circle) for a valve lift of 12 mm. Polar diagram (<b>c</b>) of gas velocity for baseline case (standard plenum), V1 plenum, and standard plenum with G2 port, along the green circle.</p>
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<p>Experimental and numerical volumetric efficiency vs. rpm by using the baseline plenum.</p>
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<p>Experimental and numerical results in terms of in-cylinder pressure at 5000 rpm (<b>a</b>), 5500 rpm (<b>b</b>), and 5800 rpm (<b>c</b>) for the baseline plenum. Red dashed line indicates EVC; blue dashed lines indicate IVO and IVC.</p>
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<p>Contour plots of burned gas mass fraction at 2500 rpm (<b>a</b>) and 5800 rpm (<b>b</b>) along the valves axis plane. In the legend, 0 stands for fresh charge and 1 for residual gas mass fractions.</p>
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<p>Computed in-cylinder fresh charge, residual gas, and total gas mass as a function of CAD at 2500 rpm (<b>a</b>), 5000 rpm (<b>b</b>), 5500 rpm (<b>c</b>), and 5800 rpm (<b>d</b>) with standard plenum. Red dashed line indicates EVC, blue dashed lines indicate IVO and IVC, and black dashed line indicates SA.</p>
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<p>Computed gas pressure in the intake manifold and in the cylinder vs. CAD at different rpms with the baseline plenum: (<b>a</b>) 2500 rpm, (<b>b</b>) 5000 rpm, (<b>c</b>) 5500 rpm, and (<b>d</b>) 5800 rpm. Red dashed line indicates EVC, blue dashed lines indicate IVO and IVC, and black dashed line indicates SA.</p>
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<p>Numerical profiles of in-cylinder total gas mass as a function of CAD at 5000 rpm (<b>a</b>), 5500 rpm (<b>b</b>), and 5800 rpm (<b>c</b>) with standard plenum and V1 plenum. Red dashed line indicates EVC, blue dashed lines indicate IVO and IVC, and black dashed line indicates SA.</p>
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<p>Computed gas pressure in the standard plenum and V1 plenum at 5000 rpm (<b>a</b>), 5500 rpm (<b>b</b>), and 5800 rpm (<b>c</b>). Red dashed line indicates EVC, blue dashed lines indicate IVO and IVC, and black dashed line indicates SA.</p>
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<p>Computed gas pressure at the probe location for the baseline case and V1 plenum at 5000 rpm (<b>a</b>) and 5800 rpm (<b>b</b>). Red dashed line indicates EVC, blue dashed lines indicate IVO and IVC, and black dashed line indicates SA.</p>
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<p>Turbulent kinetic energy in the chamber as a function of crank angle for the standard plenum and V1 plenum.</p>
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<p>Mass-average swirl ratio (SR) and tumble ratio (TR) as a function of crank angle for standard plenum and V1 plenum.</p>
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<p>Computed in-cylinder fresh charge, residual gas, and total gas mass as a function of CAD at 5800 rpm for (<b>a</b>) the baseline case and (<b>b</b>) the standard plenum with G2 port. Red dashed line indicates EVC, blue dashed lines indicate IVO and IVC, and black dashed line indicates SA.</p>
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<p>Turbulent kinetic energy in the engine chamber as a function of crank angle for the baseline case and standard plenum with G2 port.</p>
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<p>Mass-average swirl ratio (SR) and tumble ratio (TR) as a function of crank angle of the baseline case and standard plenum with G2 port.</p>
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15 pages, 312 KiB  
Article
Spinor–Vector Duality and Mirror Symmetry
by Alon E. Faraggi
Universe 2024, 10(10), 402; https://doi.org/10.3390/universe10100402 - 19 Oct 2024
Viewed by 654
Abstract
Mirror symmetry was first observed in worldsheet string constructions, and was shown to have profound implications in the Effective Field Theory (EFT) limit of string compactifications, and for the properties of Calabi–Yau manifolds. It opened up a new field in pure mathematics, and [...] Read more.
Mirror symmetry was first observed in worldsheet string constructions, and was shown to have profound implications in the Effective Field Theory (EFT) limit of string compactifications, and for the properties of Calabi–Yau manifolds. It opened up a new field in pure mathematics, and was utilised in the area of enumerative geometry. Spinor–Vector Duality (SVD) is an extension of mirror symmetry. This can be readily understood in terms of the moduli of toroidal compactification of the Heterotic String, which includes the metric the antisymmetric tensor field and the Wilson line moduli. In terms of the toroidal moduli, mirror symmetry corresponds to mappings of the internal space moduli, whereas Spinor–Vector Duality corresponds to maps of the Wilson line moduli. In the past few of years, we demonstrated the existence of Spinor–Vector Duality in the effective field theory compactifications of string theories. This was achieved by starting with a worldsheet orbifold construction that exhibited Spinor–Vector Duality and resolving the orbifold singularities, hence generating a smooth, effective field theory limit with an imprint of the Spinor–Vector Duality. Just like mirror symmetry, the Spinor–Vector Duality can be used to study the properties of complex manifolds with vector bundles. Spinor–Vector Duality offers a top-down approach to the “Swampland” program, by exploring the imprint of the symmetries of the ultra-violet complete worldsheet string constructions in the effective field theory limit. The SVD suggests a demarcation line between (2,0) EFTs that possess an ultra-violet complete embedding versus those that do not. Full article
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<p>Density plot depicting the Spinor–Vector Duality in the space of fermionic <math display="inline"><semantics> <mrow> <msub> <mi>Z</mi> <mn>2</mn> </msub> <mo>×</mo> <msub> <mi>Z</mi> <mn>2</mn> </msub> </mrow> </semantics></math> Heterotic String orbifolds. The figure shows the number of models with a given number of <math display="inline"><semantics> <mrow> <mo>(</mo> <mn>16</mn> <mo>+</mo> <mover> <mn>16</mn> <mo>¯</mo> </mover> <mo>)</mo> </mrow> </semantics></math> and 10 representations of <math display="inline"><semantics> <mrow> <mi>S</mi> <mi>O</mi> <mo>(</mo> <mn>10</mn> <mo>)</mo> </mrow> </semantics></math>. It is symmetric under the exchange of rows and columns, reflecting the SVD that underlies the entire space of vacua.</p>
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<p>The <math display="inline"><semantics> <mrow> <msub> <mi>Z</mi> <mn>2</mn> </msub> <mo>×</mo> <msubsup> <mi>Z</mi> <mn>2</mn> <mo>′</mo> </msubsup> </mrow> </semantics></math> partition function of the <math display="inline"><semantics> <msup> <mi>g</mi> <mo>′</mo> </msup> </semantics></math>-twist and <span class="html-italic">g</span> Wilson line with discrete torsion <math display="inline"><semantics> <mrow> <mi>ϵ</mi> <mo>=</mo> <mo>±</mo> <mn>1</mn> </mrow> </semantics></math>.</p>
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15 pages, 1120 KiB  
Article
Some Mathematical Examples of Emergent Intuitive Local Time Flow
by Manuel L. Esquível, Nadezhda P. Krasii and Philippe L. Didier
Foundations 2024, 4(4), 537-551; https://doi.org/10.3390/foundations4040035 - 8 Oct 2024
Viewed by 1068
Abstract
After reviewing important historical and present day ideas about the concept of time, we develop some instances of mathematical examples where, from the interaction of concepts that model interactions of things in the observable world, time flow emerges in an intuitive and local [...] Read more.
After reviewing important historical and present day ideas about the concept of time, we develop some instances of mathematical examples where, from the interaction of concepts that model interactions of things in the observable world, time flow emerges in an intuitive and local interpretation. We present several instances of emergence of time flow in mathematical contexts, to wit, by specific parametrisation of deterministic and stochastic curves or of geodesics in Riemann manifolds. Full article
(This article belongs to the Section Mathematical Sciences)
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<p>Two functions of time (<b>left</b>) and a curve in the plane where there is no unit of time (<b>right</b>); on the left-hand side, <math display="inline"><semantics> <mrow> <mi>t</mi> <mo>=</mo> <mn>0</mn> </mrow> </semantics></math> corresponds to <math display="inline"><semantics> <mrow> <mi>z</mi> <mo>(</mo> <mn>0</mn> <mo>)</mo> <mo>≈</mo> <mn>2.6</mn> </mrow> </semantics></math> and <math display="inline"><semantics> <mrow> <mi>u</mi> <mo>(</mo> <mn>0</mn> <mo>)</mo> <mo>≈</mo> <mn>4</mn> </mrow> </semantics></math>; so, on the right-hand side, the origin of the curve is the extremity of this curve, which lies in inf. class 4.</p>
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<p>A geodesic in a modified torus with equation <math display="inline"><semantics> <mrow> <mo>(</mo> <mo form="prefix">cos</mo> <mo>(</mo> <mi>u</mi> <mo>)</mo> <mo>(</mo> <mi>a</mi> <mo>+</mo> <mi>b</mi> <mo form="prefix">cos</mo> <mo>(</mo> <mi>v</mi> <mo>)</mo> <mo>)</mo> <mo>,</mo> </mrow> </semantics></math> <math display="inline"><semantics> <mrow> <mo form="prefix">sin</mo> <mo>(</mo> <mi>u</mi> <mo>)</mo> <mo>(</mo> <mi>a</mi> <mo>+</mo> <mi>b</mi> <mo form="prefix">cos</mo> <mo>(</mo> <mi>v</mi> <mo>)</mo> <mo>)</mo> <mo>,</mo> <mi>c</mi> <mo form="prefix">cos</mo> <mo>(</mo> <mi>u</mi> <mo>)</mo> <mo form="prefix">sin</mo> <mo>(</mo> <mi>v</mi> <mo>)</mo> <mo>)</mo> </mrow> </semantics></math> and parameters <math display="inline"><semantics> <mrow> <mi>a</mi> <mo>=</mo> <mn>3</mn> </mrow> </semantics></math>, <math display="inline"><semantics> <mrow> <mi>b</mi> <mo>=</mo> <mn>1</mn> </mrow> </semantics></math>, and <math display="inline"><semantics> <mrow> <mi>c</mi> <mo>=</mo> <mn>1</mn> </mrow> </semantics></math>.</p>
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<p>A 2D Wiener process single-path representation of an image that resembles a Norbert Wiener photo.</p>
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<p>An example of a stochastic line on the plane of integrated trajectories of price and volume processes of a stock.</p>
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13 pages, 3426 KiB  
Review
Phospholipid Scramblase Activity of VDAC Dimers: New Implications for Cell Death, Autophagy and Ageing
by Patrick Rockenfeller
Biomolecules 2024, 14(10), 1218; https://doi.org/10.3390/biom14101218 - 26 Sep 2024
Viewed by 1012
Abstract
Voltage-dependent anion channels (VDACs) are important proteins of the outer mitochondrial membrane (OMM). Their beta-barrel structure allows for efficient metabolite exchange between the cytosol and mitochondria. VDACs have further been implicated in the control of regulated cell death. Historically, VDACs have been pictured [...] Read more.
Voltage-dependent anion channels (VDACs) are important proteins of the outer mitochondrial membrane (OMM). Their beta-barrel structure allows for efficient metabolite exchange between the cytosol and mitochondria. VDACs have further been implicated in the control of regulated cell death. Historically, VDACs have been pictured as part of the mitochondrial permeability transition pore (MPTP). New concepts of regulated cell death involving VDACs include its oligomerisation to form a large pore complex in the OMM; however, alternative VDAC localisation to the plasma membrane has been suggested in the literature and will be discussed regarding its potential role during cell death. Very recently, a phospholipid scramblase activity has been attributed to VDAC dimers, which explains the manifold lipidomic changes observed in VDAC-deficient yeast strains. In this review, I highlight the recent advances regarding VDAC’s phospholipid scramblase function and discuss how this new insight sheds new light on VDAC’s implication in regulated cell death, autophagy, and ageing. Full article
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<p>Model of VDAC/Por1 scramblase function during autophagy. Dimeric VDAC/Por1 effectively flips PS from the cytosol-facing leaflet to the IMS-facing leaflet of the OMM through its scramblase function, as successfully flipped PS is withdrawn from the equilibrium by Psd1-mediated decarboxylation acting from the IMM in trans. PE can be re-externalised to the cytosol-facing leaflet by VDAC/Por1 scramblase activity and channelled into the ER via ER–mitochondria contact sites such as ERMES or MIA in yeast or MAMs in mammalian cells. PE situated in the outward-facing ER leaflet can be transported to autophagosomal IMs via ER exit sites (ERES) via Atg2/Atg18, which functions as a lipid channel. Atg9 scrambles phospholipids across IM leaflets.</p>
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<p>Model of potential VDAC scramblase activity in the plasma membrane during apoptosis. VDAC/Por1 is overexpressed under diverse pathological conditions associated with apoptosis. (<b>A</b>) VDAC/Por1 overexpression might trigger its implementation and dimerisation in the plasma membrane (<b>B</b>) where it could externalise PS through its phospholipid scramblase activity (magnification in (<b>C</b>)). Dashed arrows and question marks indicate hypothetical character of events.</p>
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<p>Model of potential involvement of VDAC dimer scramblase activity in mitochondrial apoptosis/mitophagy. VDAC/Por1 dimers scramble phospholipids in the OMM, which leads to the de facto import of PA from the cytosolic-facing to the intermembrane-space-facing membrane leaflet. PRELID/TRIAB transports PA from the OMM to the IMM, reducing its concentration at the IMM-facing leaflet of the OMM, which drives directed scramblase activity towards import. PA accesses the matrix-facing leaflet of the IMM via an unknown lipid scramblase or flippase. PA is converted to CL in four steps that involve choline-diphosphate-diacylglycerol (CDP-DAG), phosphatidylglycerol-phosphate (PGP), and phosphatidylglycerol (PG), and is catalysed by consecutive activity of TAM41 mitochondrial translocator assembly and maintenance homolog (TAMM41), phosphatidylglycerophosphate synthase (PGS1), protein tyrosine phosphatase mitochondrial 1 (PTPMT1), and cardiolipin synthase (CLS1). After scrambling/flipping activity (from unknown protein function), CL undergoes acyl chain remodelling by TAZ1 activity and is then transported to the intermembrane-space-facing membrane leaflet of the OMM, which depends on mitochondrial nucleoside diphosphate kinase (NDPK-D) and mitochondrial creatine kinase (MtCK). Phospholipid scramblase 3 (PLS3) enables the flipping of CL to the outer OMM leaflet, a reaction that might alternatively also be executed by VDAC dimers, as indicated by the dashed arrow and question marks.</p>
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