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Search Results (412)

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Keywords = high-speed camera measurements

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16 pages, 3623 KiB  
Article
Background Light Suppression for Multispectral Imaging in Surgical Settings
by Moritz Gerlich, Andreas Schmid, Thomas Greiner and Stefan Kray
Sensors 2025, 25(1), 141; https://doi.org/10.3390/s25010141 - 29 Dec 2024
Viewed by 378
Abstract
Multispectral imaging (MSI) enables non-invasive tissue differentiation based on spectral characteristics and has shown great potential as a tool for surgical guidance. However, adapting MSI to open surgeries is challenging. Systems that rely on light sources present in the operating room experience limitations [...] Read more.
Multispectral imaging (MSI) enables non-invasive tissue differentiation based on spectral characteristics and has shown great potential as a tool for surgical guidance. However, adapting MSI to open surgeries is challenging. Systems that rely on light sources present in the operating room experience limitations due to frequent lighting changes, which distort the spectral data and require countermeasures such as disruptive recalibrations. On the other hand, MSI systems that rely on dedicated lighting require external light sources, such as surgical lights, to be turned off during open surgery settings. This disrupts the surgical workflow and extends operation times. To this end, we present an approach that addresses these issues by combining active illumination with smart background suppression. By alternately capturing images with and without a modulated light source at a desired wavelength, we isolate the target signal, enabling artifact-free spectral scanning. We demonstrate the performance of our approach using a smart pixel camera, emphasizing its signal-to-noise ratio (SNR) advantage over a conventional high-speed camera. Our results show that accurate reflectance measurements can be achieved in clinical settings with high background illumination. Medical application is demonstrated through the estimation of blood oxygenation, and its suitability for open surgeries is discussed. Full article
(This article belongs to the Section Sensing and Imaging)
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Figure 1

Figure 1
<p>(<b>a</b>) Ximea camera (top), Heliotis C4 camera (bottom), and multispectral LED array (left); (<b>b</b>) single demodulation period of the C4 camera, subdivided into four quarter periods. Active illumination is switched on during quarter periods highlighted in orange and switched off in quarter periods depicted as black. The resulting I- and Q-components are summed internally over <span class="html-italic">n<sub>periods</sub></span> to form the in-phase and quadrature images; (<b>c</b>) operation principle of the C4 with <span class="html-italic">T</span> = 0.1 ms and <span class="html-italic">n<sub>periods</sub></span> = 12. Each sequence of duration <span class="html-italic">n<sub>periods</sub></span>·<span class="html-italic">T</span> results in one I/Q image, which is stored digitally on the camera’s internal memory. The resulting images are transferred after one burst; (<b>d</b>) background suppression as realized with the Ximea for an exposure time of 1 ms and maximal frame rate of 773 fps; (<b>e</b>) same as (<b>c</b>) with an exposure time of 100 µs. Note the dead times between frames due to the limited frame rate.</p>
Full article ">Figure 2
<p>(<b>a</b>) Setup at 56,000 lux background illumination; (<b>b</b>) spectral composition of the LED spotlights (background light); (<b>c</b>) spectral composition of the multispectral LED array; (<b>d</b>) temporal intensity of LED spotlights as measured with the photoreceiver.</p>
Full article ">Figure 3
<p>(<b>a</b>) Schematic depiction of the experimental setup. The distance of the cameras to the imaged object was fixed at 75 cm throughout this work; the distance from the LED spotlights to the target was set to be 50 cm; (<b>b</b>) color target. The white patch at the bottom left was used as the test object.</p>
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<p>Required time to record the test object with a target SNR of 10 for one spectral channel. The intensity of the active light is depicted on the <span class="html-italic">x</span>-axis. The ratio of active illumination to background light ranged from 2.4% (red arrow) down to 0.1% (black arrow).</p>
Full article ">Figure 5
<p>(<b>a</b>) C4 reconstructed RGB image. The highlighted box indicates the field of view of the Ximea camera; (<b>b</b>) C4, single-channel image with a central wavelength of 810 nm; (<b>c</b>) SNR as recorded with the C4, averaged over all channels. The SNR image was cropped to the size of the color target; (<b>d</b>) Ximea, reconstructed RGB image; (<b>e</b>) Ximea, single-channel image with a central wavelength of 810 nm; (<b>f</b>) SNR as recorded with the Ximea, averaged over all channels. The SNR image was cropped to the size of the color target; (<b>a</b>–<b>f</b>) values on the image axes denote the pixel position.</p>
Full article ">Figure 6
<p>Exemplary reflectance spectra of the color target for the dark-blue tile (<b>a</b>) and the salmon tile (<b>b</b>). Vertical bars indicate the standard deviation of pixel-wise recorded reflectance spectra. Statistics were estimated from 1000 pixel-wise reflectance spectra for each tile of the color target.</p>
Full article ">Figure 7
<p>Perfusion assessment throughout the arterial occlusion: (<b>a</b>) false color images as recorded by the C4. Images were cropped for better comparison. Values on the image axes denote the pixel position; (<b>b</b>) false color images as recorded by the Ximea. Images were cropped, and gray-level images were color-coded for enhanced visibility. Values on the image axes denote the pixel position; (<b>c</b>) color coding for the C4 as a function of tissue oxygenation. The color coding was centered at 85% SO<sub>2</sub> for the C4 and at 57% SO<sub>2</sub> for the Ximea, according to (<b>d</b>,<b>e</b>); (<b>d</b>) average pixel-wise oxygen saturation over time as recorded by the C4; (<b>e</b>) average pixel-wise oxygen saturation over time as recorded by the Ximea.</p>
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17 pages, 13925 KiB  
Article
Enhancing Weigh-in-Motion Systems Accuracy by Considering Camera-Captured Wheel Oscillations
by Moritz P. M. Hagmanns, Serge Lamberty, Adrian Fazekas and Markus Oeser
Sensors 2024, 24(24), 8151; https://doi.org/10.3390/s24248151 - 20 Dec 2024
Viewed by 239
Abstract
Weigh-in-motion (WIM) systems aim to estimate a vehicle’s weight by measuring static wheel loads as it passes at highway speed over roadway-embedded sensors. Vehicle oscillations and the resulting dynamic load components are critical factors affecting measurements and limiting accuracy. As of now, a [...] Read more.
Weigh-in-motion (WIM) systems aim to estimate a vehicle’s weight by measuring static wheel loads as it passes at highway speed over roadway-embedded sensors. Vehicle oscillations and the resulting dynamic load components are critical factors affecting measurements and limiting accuracy. As of now, a satisfactory solution has yet to be found. This paper discusses a novel correction approach that fuses WIM sensor data with wheel oscillation captured by cameras. In an experiment, a hard plastic speed bump was placed ahead of a piezoelectric WIM sensor to induce oscillation in trucks crossing the WIM sensor. Three high-speed cameras captured the motion of the wheels. The results show that the proposed method improved the accuracy of the measured gross weight for significant wheel oscillations, while no improvement is observed for smaller oscillation amplitudes. Full article
(This article belongs to the Section Vehicular Sensing)
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Figure 1

Figure 1
<p>Experimental setup on the German A61 highway used to gather data. A truck is about to cross the speed bump, followed by the WIM sensors. A laser sensor triggers the recordings of the three industrial-grade cameras.</p>
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<p>Vehicles utilized for measurement runs: truck with trailer (<b>a</b>), truck without trailer (<b>b</b>), and semitrailer (<b>c</b>).</p>
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<p>Collage of six example images as a truck passes by. The top row (<b>a</b>–<b>c</b>) and the bottom row (<b>d</b>–<b>f</b>) consist of three images taken by the three cameras simultaneously and their Hough-transformed images, respectively. It can be seen, how the center of the wheel creates a white spot in the Hough image (<b>e</b>).</p>
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<p>Tracking of the wheel center. The pattern from the Hough transform (<b>a</b>) is correlated (operation is denoted with a star symbol *) as a moving window with the timely next consecutive image (<b>b</b>), resulting in a heat map indicating where the pattern can be found in the new image (<b>c</b>). The local maxima was selected as the new wheel’s center position.</p>
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<p>Example for the oscillation of the wheels: 150 cm bump spacing (<b>a</b>), without bump (<b>b</b>). The deflection A of the wheel at the sensor is depicted visually. The <span class="html-italic">j</span> th data point is marked for the 150 cm bump spacing.</p>
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<p>Determination of the correction function (linear regression).</p>
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<p>Wheel loses contact with the ground after crossing the speed bump and even misses the sensor.</p>
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<p>Comparison of the WIM-measured uncorrected and corrected total weights <span class="html-italic">M</span> with their reference gross weights <span class="html-italic">R</span> for 150 cm bump spacing (<b>a</b>) and without bump (<b>b</b>).</p>
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12 pages, 3681 KiB  
Article
Influence of Wind Speed on the Motion Characteristics of Peach Leaves (Prunus persica)
by Guanqun Wang, Xiang Dong, Weidong Jia, Mingxiong Ou, Pengpeng Yu, Minmin Wu, Zhi Zhang, Xinkang Hu, Yourui Huang and Fengxiang Lu
Agriculture 2024, 14(12), 2307; https://doi.org/10.3390/agriculture14122307 - 16 Dec 2024
Viewed by 470
Abstract
Air-assisted sprayers are widely used in orchards due to their efficiency in enhancing droplet penetration and deposition. These sprayers disperse droplets through a high-velocity airflow, which agitates the leaves and aids in canopy penetration. This study involved controlled experiments to simulate leaf movement [...] Read more.
Air-assisted sprayers are widely used in orchards due to their efficiency in enhancing droplet penetration and deposition. These sprayers disperse droplets through a high-velocity airflow, which agitates the leaves and aids in canopy penetration. This study involved controlled experiments to simulate leaf movement during field spraying, with a focus on the dynamics of peach tree leaves (Prunus persica) in varying wind fields. An experimental setup consisting of a wind-conveying system, a measurement system, and a fixed system was designed. The moving speeds of the wind field (0.75 m/s, 0.5 m/s, and 1.0 m/s) and wind velocities (ranging from 2 m/s to 8 m/s) were varied. Key parameters, including leaf tip displacement, angular velocity, and twisting amplitude, were measured using high-speed cameras and motion analysis software. The results indicate that, at a constant wind velocity, increasing the wind field’s moving speed resulted in a reduced range of motion, decelerated angular velocity, and decreased twisting amplitude of the leaves. Notably, at a wind field speed of 8 m/s and a moving speed of 1.0 m/s, the twisting duration of the leaves was only 67% of that observed at a moving speed of 0.5 m/s. These findings suggest that wind speed and field motion characteristics play a crucial role in leaf dynamics, informing the design of air-assisted spraying systems. Full article
(This article belongs to the Section Agricultural Technology)
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Figure 1
<p>Experimental platform.</p>
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<p>Moving beam and wind speed: (<b>a</b>) Moving beam direction indication; (<b>b</b>) Distribution of wind speed.</p>
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<p>X-direction displacement of leaf tip under different moving speeds and wind speeds, (<b>a</b>) movement speed 0.5 m/s; (<b>b</b>) movement speed 0.75 m/s; (<b>c</b>) movement speed 1.0 m/s.</p>
Full article ">Figure 4
<p>Y-direction displacement of leaf tip under different moving speeds and wind speeds, (<b>a</b>) movement speed 0.5 m/s; (<b>b</b>) movement speed 0.75 m/s; (<b>c</b>) movement speed 1.0 m/s.</p>
Full article ">Figure 5
<p>Angular velocity of leaf tip under different moving speeds and wind speeds, (<b>a</b>) movement speed 0.5 m/s; (<b>b</b>) movement speed 0.75 m/s; (<b>c</b>) movement speed 1.0 m/s.</p>
Full article ">Figure 6
<p>Comparison of the maximum leaf flip angle with the initial state of flipping. (<b>a</b>) Beam speed 0.5 m/s, (<b>b</b>) Beam speed 1.0 m/s.</p>
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17 pages, 5301 KiB  
Article
Combined Dielectric-Optical Characterization of Single Cells Using Dielectrophoresis-Imaging Flow Cytometry
by Behnam Arzhang, Justyna Lee, Emerich Kovacs, Michael Butler, Elham Salimi, Douglas J. Thomson and Greg E. Bridges
Biosensors 2024, 14(12), 577; https://doi.org/10.3390/bios14120577 - 27 Nov 2024
Viewed by 933
Abstract
In this paper, we present a microfluidic flow cytometer for simultaneous imaging and dielectric characterization of individual biological cells within a flow. Utilizing a combination of dielectrophoresis (DEP) and high-speed imaging, this system offers a dual-modality approach to analyze both cell morphology and [...] Read more.
In this paper, we present a microfluidic flow cytometer for simultaneous imaging and dielectric characterization of individual biological cells within a flow. Utilizing a combination of dielectrophoresis (DEP) and high-speed imaging, this system offers a dual-modality approach to analyze both cell morphology and dielectric properties, enhancing the ability to analyze, characterize, and discriminate cells in a heterogeneous population. A high-speed camera is used to capture images of and track multiple cells in real-time as they flow through a microfluidic channel. A wide channel is used, enabling analysis of many cells in parallel. A coplanar electrode array perpendicular to cell flow is incorporated at the bottom of the channel to perform dielectrophoresis-based dielectric characterization. A frequency-dependent voltage applied to the array produces a non-uniform electric field, translating cells to higher or lower velocity depending on their dielectric polarizability. In this paper, we demonstrate how cell size, obtained by optical imaging, and DEP response, obtained by particle tracking, can be used to discriminate viable and non-viable Chinese hamster ovary cells in a heterogeneous cell culture. Multiphysics electrostatic-fluid dynamics simulation is used to develop a relationship between cell incoming velocity, differential velocity, size, and the cell’s polarizability, which can subsequently be used to evaluate its physiological state. Measurement of a mixture of polystyrene microspheres is used to evaluate the accuracy of the cytometer. Full article
(This article belongs to the Special Issue Biosensing Applications for Cell Monitoring)
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Figure 1

Figure 1
<p>(<b>a</b>) Experimental setup of the DEP-imaging flow cytometer. (<b>b</b>) Microfluidic chip, fluid delivery, and interface for DEP. (<b>c</b>) Schematic diagram of the DEP-imaging flow cytometer, comprising camera, light source, and microfluidic channel sandwiched between glass slides with fluid inlet ports. (<b>d</b>) Longitudinal cross-section indicating cell trajectory in a parabolic laminar flow and showing height and velocity change induced by DEP actuation due to the non-uniform field above coplanar electrodes.</p>
Full article ">Figure 2
<p>Optical capture and analysis of cells. Background subtraction, contrast enhancement, bright spot elimination, and cell visibility enhancement are used to track cells and identify key cell features. (<b>a</b>) Example of one gray-scaled video frame. The CHO cell in the inset is 23.7 pixels across (the electrodes are manually added in this plot). (<b>b</b>) The trajectory of cells is plotted based on data obtained by the tracking algorithm. (<b>c</b>) Tracking data are used to plot position vs time and find the cell’s velocity before and after the electrode.</p>
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<p>(<b>a</b>) Double-shell model of a CHO cell with radius <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>r</mi> </mrow> <mrow> <mi>c</mi> <mi>e</mi> <mi>l</mi> <mi>l</mi> </mrow> </msub> </mrow> </semantics></math>. (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>R</mi> <mi>e</mi> <mfenced open="{" close="}" separators="|"> <mrow> <msub> <mrow> <mi>K</mi> </mrow> <mrow> <mi>c</mi> <mi>m</mi> </mrow> </msub> <mo>(</mo> <mi>ω</mi> <mo>)</mo> </mrow> </mfenced> </mrow> </semantics></math> spectra for viable and non-viable CHO cells in a medium with <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>σ</mi> </mrow> <mrow> <mi>m</mi> <mi>e</mi> <mi>d</mi> </mrow> </msub> <mo>=</mo> <mn>0.17</mn> <mo> </mo> <mi mathvariant="normal">S</mi> <mo>/</mo> <mi mathvariant="normal">m</mi> </mrow> </semantics></math> and <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>ε</mi> </mrow> <mrow> <mi>m</mi> <mi>e</mi> <mi>d</mi> </mrow> </msub> <mo>=</mo> <mn>78</mn> <mo> </mo> <msub> <mrow> <mi>ε</mi> </mrow> <mrow> <mn>0</mn> </mrow> </msub> </mrow> </semantics></math>. Nominal size and electrical parameters are taken from [<a href="#B42-biosensors-14-00577" class="html-bibr">42</a>] and provided in <a href="#biosensors-14-00577-t001" class="html-table">Table 1</a>. The red regions show the effect of <math display="inline"><semantics> <mrow> <mo>±</mo> <mn>20</mn> <mo>%</mo> </mrow> </semantics></math> variation in the cell size (<math display="inline"><semantics> <mrow> <msub> <mrow> <mi>r</mi> </mrow> <mrow> <mi>c</mi> <mi>e</mi> <mi>l</mi> <mi>l</mi> </mrow> </msub> <mo>=</mo> <mn>5</mn> <mo>–</mo> <mn>7.5</mn> <mo> </mo> <mi mathvariant="normal">m</mi> </mrow> </semantics></math> for viable cells and <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>r</mi> </mrow> <mrow> <mi>c</mi> <mi>e</mi> <mi>l</mi> <mi>l</mi> </mrow> </msub> <mo>=</mo> <mn>4.5</mn> <mo>–</mo> <mn>7</mn> <mo> </mo> <mi mathvariant="normal">m</mi> </mrow> </semantics></math> for non-viable cells). The cyan regions show the effect of <math display="inline"><semantics> <mrow> <mo>±</mo> <mn>20</mn> <mo>%</mo> </mrow> </semantics></math> variation in the cytoplasm conductivity (<math display="inline"><semantics> <mrow> <msub> <mrow> <mi>σ</mi> </mrow> <mrow> <mi mathvariant="normal">c</mi> <mi mathvariant="normal">y</mi> <mi mathvariant="normal">t</mi> </mrow> </msub> <mo>=</mo> <mn>0.43</mn> <mo>−</mo> <mn>0.63</mn> <mo> </mo> <mi mathvariant="normal">S</mi> <mo>/</mo> <mi mathvariant="normal">m</mi> </mrow> </semantics></math> for viable cells and <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>σ</mi> </mrow> <mrow> <mi mathvariant="normal">c</mi> <mi mathvariant="normal">y</mi> <mi mathvariant="normal">t</mi> </mrow> </msub> <mo>=</mo> <mn>0.055</mn> <mo>−</mo> <mn>0.085</mn> <mo> </mo> <mi mathvariant="normal">S</mi> <mo>/</mo> <mi mathvariant="normal">m</mi> </mrow> </semantics></math> for non-viable cells). The dashed line shows <math display="inline"><semantics> <mrow> <mi>R</mi> <mi>e</mi> <mfenced open="{" close="}" separators="|"> <mrow> <msub> <mrow> <mi>K</mi> </mrow> <mrow> <mi>c</mi> <mi>m</mi> </mrow> </msub> <mo>(</mo> <mi>ω</mi> <mo>)</mo> </mrow> </mfenced> </mrow> </semantics></math> for a 15.7 µm diameter PSS with <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>ε</mi> </mrow> <mrow> <mi>r</mi> <mi>b</mi> </mrow> </msub> <mo> </mo> <mo>=</mo> <mo> </mo> <mn>2.5</mn> </mrow> </semantics></math> and surface conductance, <math display="inline"><semantics> <mrow> <msub> <mi>K</mi> <mrow> <mi>s</mi> <mi>u</mi> <mi>r</mi> <mi>f</mi> </mrow> </msub> <mo> </mo> <mo>=</mo> <mo> </mo> <mn>1</mn> </mrow> </semantics></math> nS in a DI water medium [<a href="#B57-biosensors-14-00577" class="html-bibr">57</a>].</p>
Full article ">Figure 4
<p>Differential velocity <math display="inline"><semantics> <mrow> <msub> <mrow> <mo>(</mo> <mi>v</mi> </mrow> <mrow> <mi mathvariant="normal">i</mi> </mrow> </msub> <mo>−</mo> <msub> <mrow> <mi>v</mi> </mrow> <mrow> <mi mathvariant="normal">o</mi> </mrow> </msub> <mo>)</mo> </mrow> </semantics></math> versus incoming velocity for a mixture of 10 µm (blue) and 15.7 µm (red) polystyrene microspheres at V<sub>DEP</sub> = 6 V<sub>pp</sub> and f = 1 MHz. Data points are colored according to optically measured size (see <a href="#biosensors-14-00577-f005" class="html-fig">Figure 5</a>).</p>
Full article ">Figure 5
<p>Particle size distribution for imaged 10 µm (blue) and 15.7 µm (red) diameter PSS corresponding to the colored data points in <a href="#biosensors-14-00577-f004" class="html-fig">Figure 4</a>.</p>
Full article ">Figure 6
<p>Simulation of the differential velocity, <math display="inline"><semantics> <mrow> <msub> <mrow> <mo>(</mo> <mi>v</mi> </mrow> <mrow> <mi mathvariant="normal">i</mi> </mrow> </msub> <mo>−</mo> <msub> <mrow> <mi>v</mi> </mrow> <mrow> <mi mathvariant="normal">o</mi> </mrow> </msub> <mo>)</mo> </mrow> </semantics></math>, as a function of incoming velocity, <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>v</mi> </mrow> <mrow> <mi>i</mi> </mrow> </msub> </mrow> </semantics></math>, for cells with diameters and Clausius-Mossotti factor values typical of (<b>a</b>) viable and (<b>b</b>) non-viable cells. A 20% variation in <math display="inline"><semantics> <mrow> <mi>R</mi> <mi>e</mi> <mfenced open="{" close="}" separators="|"> <mrow> <msub> <mrow> <mi>K</mi> </mrow> <mrow> <mi>c</mi> <mi>m</mi> </mrow> </msub> </mrow> </mfenced> </mrow> </semantics></math> and size is evaluated.</p>
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<p>Scatter plot of differential velocity versus incoming velocity for CHO cells for a DEP frequency of 6 MHz. A Gaussian mixture model clustering algorithm is used to separate CHO cell populations into viable (blue) and non-viable (red) clusters. The bars indicate the simulated variation due to 20% variability in cell size and <math display="inline"><semantics> <mrow> <mi>R</mi> <mi>e</mi> <mfenced open="{" close="}" separators="|"> <mrow> <msub> <mrow> <mi>K</mi> </mrow> <mrow> <mi>c</mi> <mi>m</mi> </mrow> </msub> </mrow> </mfenced> </mrow> </semantics></math>.</p>
Full article ">Figure 8
<p>Size distributions for viable and non-viable CHO cells, as obtained by combining the cluster data in <a href="#biosensors-14-00577-f007" class="html-fig">Figure 7</a> at 6 MHz and in <a href="#biosensors-14-00577-f0A1" class="html-fig">Figure A1</a> at 3 MHz.</p>
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<p>Size distributions for CHO-EG2 cells measured by a cell counter. A viability of 70% was measured using trypan blue assay.</p>
Full article ">Figure A1
<p>Scatter plot of differential velocity versus incoming velocity for CHO cells for a DEP frequency of 3 MHz. A Gaussian mixture model clustering algorithm is used to segregate CHO cell populations into viable (blue) and non-viable (red) clusters.</p>
Full article ">Figure A2
<p>Differential velocity versus incoming velocity for CHO cells when <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>V</mi> </mrow> <mrow> <mi>D</mi> <mi>E</mi> <mi>P</mi> </mrow> </msub> <mo>=</mo> <mn>0</mn> <mo> </mo> <mi mathvariant="normal">V</mi> </mrow> </semantics></math> (no DEP).</p>
Full article ">
20 pages, 8023 KiB  
Article
Reaction-Engineering Approach for Stable Rotating Glow-to-Arc Plasma—Key Principles of Effective Gas-Conversion Processes
by Samuel Jaro Kaufmann, Haripriya Chinnaraj, Johanna Buschmann, Paul Rößner and Kai Peter Birke
Catalysts 2024, 14(12), 864; https://doi.org/10.3390/catal14120864 - 26 Nov 2024
Viewed by 505
Abstract
This work presents advancements in a rotating glow-to-arc plasma reactor, designed for stable gas conversion of robust molecules like CO2, N2, and CH4. Plasma-based systems play a critical role in Power-to-X research, offering electrified, sustainable pathways for [...] Read more.
This work presents advancements in a rotating glow-to-arc plasma reactor, designed for stable gas conversion of robust molecules like CO2, N2, and CH4. Plasma-based systems play a critical role in Power-to-X research, offering electrified, sustainable pathways for industrial gas conversion. Here, we scaled the reactor’s power from 200 W to 1.2 kW in a CO2 plasma, which introduced instability due to uplift forces and arc behavior. These were mitigated by integrating silicon carbide (SiC) ceramic foam as a mechanical restriction, significantly enhancing stability by reducing arc movement, confining convection, and balancing volumetric flow within the arc. Using high-speed camera analysis and in situ electronic frequency measurements, we identified dominant frequencies tied to operational parameters, supporting potential in operando monitoring and control. Arc-rotation frequencies from 5 to 50 Hz and higher frequencies (500 to 2700 Hz) related to arc chattering reveal the system’s dynamic response to power and flow changes. Furthermore, refining the specific energy input (SEI) to account for plasma residence time allowed for a more precise calculation of effective SEI, optimizing energy delivery to target molecules. Our findings underscore the reactor’s promise for scalable, efficient gas conversion in sustainable energy applications. Full article
(This article belongs to the Special Issue Plasma Catalysis for Environment and Energy Applications)
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Figure 1

Figure 1
<p>Force balance on arc at plasma reactor with stream direction top to bottom.</p>
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<p>Uplift and gas drag force on the plasma arc plotted over the diameter <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>d</mi> </mrow> <mrow> <mi mathvariant="normal">c</mi> <mi mathvariant="normal">a</mi> <mi mathvariant="normal">t</mi> <mi mathvariant="normal">h</mi> <mi mathvariant="normal">o</mi> <mi mathvariant="normal">d</mi> <mi mathvariant="normal">e</mi> </mrow> </msub> </mrow> </semantics></math> of the cathode at various volume flows <math display="inline"><semantics> <mrow> <mover accent="true"> <mrow> <mi>V</mi> </mrow> <mo>˙</mo> </mover> </mrow> </semantics></math>.</p>
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<p>Instabilities of plasma power: Power over time (<b>f</b>); arc phenomena (right): (<b>a</b>) arc chattering; (<b>b</b>) breakdown; (<b>c</b>) shortcut; (<b>d</b>) and (<b>e</b>) spiralizing.</p>
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<p>Timesteps of arc phenomena shortcut and arc chattering at operating conditions of <math display="inline"><semantics> <mrow> <mi>B</mi> <mo>=</mo> <mn>4.5</mn> <mo> </mo> <mi mathvariant="normal">m</mi> <mi mathvariant="normal">T</mi> </mrow> </semantics></math>, <math display="inline"><semantics> <mrow> <mover accent="true"> <mrow> <mi>V</mi> </mrow> <mo>˙</mo> </mover> <mo>=</mo> <mn>2</mn> <mo> </mo> <mi>S</mi> <mi>L</mi> <mi>M</mi> </mrow> </semantics></math>, and <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>U</mi> </mrow> <mrow> <mi>i</mi> <mi>n</mi> </mrow> </msub> <mo>=</mo> <mn>500</mn> <mo> </mo> <mi mathvariant="normal">V</mi> </mrow> </semantics></math>.</p>
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<p>Silicon carbide ceramic foam included in the reactor.</p>
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<p>Plasma stability without SiC and with SiC at a magnetic flux density of <math display="inline"><semantics> <mrow> <mi>B</mi> <mo>=</mo> <mn>4.5</mn> <mo> </mo> <mi mathvariant="normal">m</mi> <mi mathvariant="normal">T</mi> </mrow> </semantics></math>, a volume flow of <math display="inline"><semantics> <mrow> <mover accent="true"> <mrow> <mi>V</mi> </mrow> <mo>˙</mo> </mover> <mo>=</mo> <mn>2</mn> <mo> </mo> <mi mathvariant="normal">S</mi> <mi mathvariant="normal">L</mi> <mi mathvariant="normal">M</mi> <mo>,</mo> </mrow> </semantics></math> and at input voltages of <math display="inline"><semantics> <mrow> <mi>U</mi> <mo>=</mo> <mn>300</mn> <mo>…</mo> <mn>500</mn> <mo> </mo> <mi mathvariant="normal">V</mi> </mrow> </semantics></math>.</p>
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<p>Plasma stability without SiC and with SiC for different operating conditions.</p>
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<p>Changes in plasma power and rotational arc frequency at different magnetic flux densities, mass flow, and voltages.</p>
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<p>Arc tracing through SiC at different magnetic fields, voltages, and mass flows. The conditions lead to rotational frequencies of (<b>a</b>) 11 Hz at 7 mT, 6 SLM, and 300 V; (<b>b</b>) 18 Hz at 7 mT, 6 SLM, and 500 V; (<b>c</b>) 36 Hz at 9.5 mT, 6 SLM, and 500 V; and (<b>d</b>) 46 Hz at 9.5 mT, 10 SLM, and 500 V.</p>
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<p>Curve of <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>I</mi> </mrow> <mrow> <mi mathvariant="normal">p</mi> <mi mathvariant="normal">l</mi> <mi mathvariant="normal">a</mi> <mi mathvariant="normal">s</mi> <mi mathvariant="normal">m</mi> <mi mathvariant="normal">a</mi> </mrow> </msub> </mrow> </semantics></math> with stable operating conditions (9.5 mT, 6 SLM, and 500 V), measured with the current probe and FFT spectrum (right), plotting the signal amplitude over the frequency.</p>
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<p>Curve of <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>I</mi> </mrow> <mrow> <mi mathvariant="normal">p</mi> <mi mathvariant="normal">l</mi> <mi mathvariant="normal">a</mi> <mi mathvariant="normal">s</mi> <mi mathvariant="normal">m</mi> <mi mathvariant="normal">a</mi> </mrow> </msub> </mrow> </semantics></math> over the first 100 ms of an experiment for different magnetic flux densities <math display="inline"><semantics> <mrow> <mi>B</mi> <mo>=</mo> <mn>4.5</mn> <mo>…</mo> <mn>9.5</mn> <mo> </mo> <mi mathvariant="normal">m</mi> <mi mathvariant="normal">T</mi> </mrow> </semantics></math> at <math display="inline"><semantics> <mrow> <mi>V</mi> <mo>=</mo> <mn>6</mn> <mo> </mo> <mi mathvariant="normal">S</mi> <mi mathvariant="normal">L</mi> <mi mathvariant="normal">M</mi> </mrow> </semantics></math>, and <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>U</mi> </mrow> <mrow> <mi>i</mi> <mi>n</mi> </mrow> </msub> <mo>=</mo> <mn>500</mn> <mo> </mo> <mi mathvariant="normal">V</mi> </mrow> </semantics></math>.</p>
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<p>Spectral power density at different variations in magnetic flux density, volume flow, and input voltage.</p>
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<p>Spectral power density at different variations in the humidity (<b>left</b>) and the dominant frequencies over the humidity (<b>right</b>).</p>
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<p>Arc images of experiments with different operating conditions with noted arc diameters.</p>
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<p>Changes in specific energy input and the number of theoretical arc contacts with molecules at different magnetic flux densities, mass flow, and voltages.</p>
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<p>Experimental setup. Electrical components: plasma driver, DC power supply. Reactor components: electrodes, magnet holder, mass flow controller. Analytical components: oscilloscope, current probe, high-speed camera.</p>
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<p>(<b>a</b>) Voltage–current graph with discharge modes; (<b>b</b>) equivalent electrical circuit.</p>
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18 pages, 3847 KiB  
Article
EC-WAMI: Event Camera-Based Pose Optimization in Remote Sensing and Wide-Area Motion Imagery
by Isaac Nkrumah, Maryam Moshrefizadeh, Omar Tahri, Erik Blasch, Kannappan Palaniappan and Hadi AliAkbarpour
Sensors 2024, 24(23), 7493; https://doi.org/10.3390/s24237493 - 24 Nov 2024
Viewed by 710
Abstract
In this paper, we present EC-WAMI, the first successful application of neuromorphic event cameras (ECs) for Wide-Area Motion Imagery (WAMI) and Remote Sensing (RS), showcasing their potential for advancing Structure-from-Motion (SfM) and 3D reconstruction across diverse imaging scenarios. ECs, which detect asynchronous [...] Read more.
In this paper, we present EC-WAMI, the first successful application of neuromorphic event cameras (ECs) for Wide-Area Motion Imagery (WAMI) and Remote Sensing (RS), showcasing their potential for advancing Structure-from-Motion (SfM) and 3D reconstruction across diverse imaging scenarios. ECs, which detect asynchronous pixel-level brightness changes, offer key advantages over traditional frame-based sensors such as high temporal resolution, low power consumption, and resilience to dynamic lighting. These capabilities allow ECs to overcome challenges such as glare, uneven lighting, and low-light conditions that are common in aerial imaging and remote sensing, while also extending UAV flight endurance. To evaluate the effectiveness of ECs in WAMI, we simulate event data from RGB WAMI imagery and integrate them into SfM pipelines for camera pose optimization and 3D point cloud generation. Using two state-of-the-art SfM methods, namely, COLMAP and Bundle Adjustment for Sequential Imagery (BA4S), we show that although ECs do not capture scene content like traditional cameras, their spike-based events, which only measure illumination changes, allow for accurate camera pose recovery in WAMI scenarios even in low-framerate(5 fps) simulations. Our results indicate that while BA4S and COLMAP provide comparable accuracy, BA4S significantly outperforms COLMAP in terms of speed. Moreover, we evaluate different feature extraction methods, showing that the deep learning-based LIGHTGLUE descriptor consistently outperforms traditional handcrafted descriptors by providing improved reliability and accuracy of event-based SfM. These results highlight the broader potential of ECs in remote sensing, aerial imaging, and 3D reconstruction beyond conventional WAMI applications. Our dataset will be made available for public use. Full article
(This article belongs to the Section Physical Sensors)
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<p>Block diagram of our EC-WAMI pipeline. RGB event data are simulated using an event simulator and frames are reconstructed with a frame reconstructor. The reconstructed frames are then fed into an SfM algorithm for camera pose optimization and 3D reconstruction.</p>
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<p>Conventional (e.g., COLMAP) versus BA4S SfM pipelines [<a href="#B15-sensors-24-07493" class="html-bibr">15</a>]. In the conventional SfM pipeline (<b>a</b>), camera poses and outliers are simultaneously estimated using RANSAC, and metadata may be used as extra constraints in optimization. In BA4S (<b>b</b>), camera metadata are used directly, and there is no model estimation, explicit outlier elimination, or RANSAC filtering of mismatches.</p>
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<p>RGB sample frames in our WAMI datasets: Top, ABQ-215; Bottom, DIRSIG-RIT. The second column illustrates events simulated with Video-to-Event (V2E), while the third column shows the reconstructed frames from events simulated with Event-to-Video (E2VID).</p>
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<p>Errors of the recovered camera poses when using BA4S and COLMAP on the two aerial image sequences: (<b>a</b>) positional error (percentage in meters, using (<a href="#FD7-sensors-24-07493" class="html-disp-formula">7</a>)) and (<b>b</b>) angular error (degrees, using (<a href="#FD9-sensors-24-07493" class="html-disp-formula">9</a>)). LIGHTGLUE outperforms other feature descriptors in terms of both the positional and angular error metrics; in contrast, ORB shows comparatively lower performance and trails in terms of both measures.</p>
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<p>Recovered camera trajectories compared to ground truth for the eABQ-215 and eRIT datasets consisting of frames extracted from simulated event data. The recovered 3D trajectories closely match the ground truth.</p>
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<p>Recovered camera trajectories in 2D, showing the differences between BA4S and COLMAP on aerial images. The top row shows the trajectory and difference for the eABQ-215 dataset, while the second row illustrates the same results for the eRIT dataset. These graphs correspond to the 3D trajectories shown in <a href="#sensors-24-07493-f005" class="html-fig">Figure 5</a>. BA4S displays a smoother trajectory, while COLMAP has a more jagged trajectory. There is a small difference between the ground truth and the optimized camera poses based on the reconstructed frames generated from simulated WAMI event data, demonstrating the effectiveness of our approach; <a href="#sensors-24-07493-t002" class="html-table">Table 2</a> provides additional details. In (<b>a</b>), the optimized trajectory for the eABQ-215 dataset; (<b>b</b>), the difference between the optimized trajectory for eABQ-215 and the ground truth; (<b>c</b>), the optimized trajectory for the eRIT dataset; (<b>d</b>), the difference between the optimized trajectory for eRIT and the ground truth.</p>
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<p>Sparse and dense 3D point clouds produced using the two SfM pipelines on the eABQ-215 and eRIT event camera datasets. The top two rows show the point clouds for eABQ-215 and the bottom two rows show the point clouds for eRIT. The results demonstrate that Gaussian splatting (GS) produces high-quality 3D scene reconstructions on both event datasets.</p>
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<p>Camera pose recovery with a traditional RGB camera in a challenging illumination scenario: (<b>a</b>) shows a simulated RGB image with perturbations generated by applying techniques from [<a href="#B51-sensors-24-07493" class="html-bibr">51</a>] to the RGB image in <a href="#sensors-24-07493-f003" class="html-fig">Figure 3</a>a, while (<b>b</b>,<b>c</b>) depict failed camera trajectory recovery when the perturbed traditional image was used as input for BA4S and COLMAP. These results underscore the limitations of traditional cameras in recovering pose under challenging illumination conditions.</p>
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16 pages, 3034 KiB  
Article
Kinematic and Aerodynamic Analysis of a Coccinella septempunctata Performing Banked Turns in Climbing Flight
by Lili Yang, Zhifei Fang and Huichao Deng
Biomimetics 2024, 9(12), 720; https://doi.org/10.3390/biomimetics9120720 - 22 Nov 2024
Viewed by 583
Abstract
Many Coccinella septempunctata flights, with their precise positioning capabilities, have provided rich inspiration for designing insect-styled micro air vehicles. However, researchers have not widely studied their flight ability. In particular, research on the maneuverability of Coccinella septempunctata using integrated kinematics and aerodynamics is [...] Read more.
Many Coccinella septempunctata flights, with their precise positioning capabilities, have provided rich inspiration for designing insect-styled micro air vehicles. However, researchers have not widely studied their flight ability. In particular, research on the maneuverability of Coccinella septempunctata using integrated kinematics and aerodynamics is scarce. Using three orthogonally positioned high-speed cameras, we captured the Coccinella septempunctata’s banking turns in the climbing flight in the laboratory. We used the measured wing kinematics in a Navier–Stokes solver to compute the aerodynamic forces acting on the insects in five cycles. Coccinella septempunctata can rapidly climb and turn during phototaxis or avoidance of predators. During banked turning in climbing flight, the translational part of the body, and the distance flown forward and upward, is much greater than the distance flown to the right. The rotational part of the body, through banking and manipulating the amplitude of the insect flapping angle, the stroke deviation angle, and the rotation angle, actively creates the asymmetrical lift and drag coefficients of the left and right wings to generate right turns. By implementing banked turns during the climbing flight, the insect can adjust its flight path more flexibly to both change direction and maintain or increase altitude, enabling it to effectively avoid obstacles or track moving targets, thereby saving energy to a certain extent. This strategy is highly beneficial for insects flying freely in complex environments. Full article
(This article belongs to the Special Issue Bio-Inspired Fluid Flows and Fluid Mechanics)
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<p>Trinocular Stereo Vision System Model.</p>
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<p>Videos of <span class="html-italic">Coccinella septempunctata</span> in climbing motion, presented from the perspectives of three cameras. The time notations are non-dimensionalized for the cycle.</p>
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<p>Reference coordinate system (<span class="html-italic">x</span><sub>E</sub>, <span class="html-italic">y<sub>E</sub></span>, <span class="html-italic">z<sub>E</sub></span>) and the body angular velocity components along the three axes of the body-fixed frame (<span class="html-italic">x<sub>b</sub></span>, <span class="html-italic">y<sub>b</sub></span>, <span class="html-italic">z<sub>b</sub></span>): <span class="html-italic">p</span> (roll rate), <span class="html-italic">q</span> (pitch rate), <span class="html-italic">r</span> (yaw rate).</p>
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<p>Wing kinematics parameters and coordinates.</p>
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<p>Turning radius of a <span class="html-italic">Coccinella septempunctata</span> on the <span class="html-italic">XY</span> plane.</p>
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<p>Portions of a computational grid system.</p>
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<p>Illustrates the temporal evolution of the lift coefficient (CL) during the banked turn in the climbing flight for <span class="html-italic">Coccinella septempunctata</span> across different grid numbers within one cycle.</p>
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<p>Variations in Euler angles (<b>a</b>) and center of mass displacement (<b>b</b>) of a <span class="html-italic">Coccinella septempunctata</span> during a banking turn.</p>
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<p>Temporal records of the movements of the <span class="html-italic">Coccinella septempunctata</span>’s body, illustrated as the (<b>a</b>) rates of Euler angles; (<b>b</b>) rates of roll, pitch, and yaw movements; and (<b>c</b>) movement speed of the body’s center of mass, detailing <span class="html-italic">u</span><sub>c</sub>, <span class="html-italic">v</span><sub>c</sub>, and <span class="html-italic">w</span><sub>c</sub> for the translational velocity components and <span class="html-italic">x</span><sub>E</sub>, <span class="html-italic">y</span><sub>E</sub>, <span class="html-italic">z</span><sub>E</sub> for the spatial velocity components of the body’s mass center.</p>
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<p>Temporal records of the movements of the <span class="html-italic">Coccinella septempunctata</span>’s body, illustrated as the (<b>a</b>) rates of Euler angles; (<b>b</b>) rates of roll, pitch, and yaw movements; and (<b>c</b>) movement speed of the body’s center of mass, detailing <span class="html-italic">u</span><sub>c</sub>, <span class="html-italic">v</span><sub>c</sub>, and <span class="html-italic">w</span><sub>c</sub> for the translational velocity components and <span class="html-italic">x</span><sub>E</sub>, <span class="html-italic">y</span><sub>E</sub>, <span class="html-italic">z</span><sub>E</sub> for the spatial velocity components of the body’s mass center.</p>
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<p>Instantaneous wing kinematics of <span class="html-italic">Coccinella septempunctata</span>, (<b>a</b>) <span class="html-italic">ϕ</span><sub>w</sub>, the flapping angle; (<b>b</b>) <span class="html-italic">θ</span><sub>w</sub>, the deviation angle; and (<b>c</b>) <span class="html-italic">α</span><sub>w,</sub> the pitching angle.</p>
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<p>Diagram illustrating insects performing inclined turns at the center of mass.</p>
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<p>Diagram illustrating insects performing inclined turns at the center of mass.</p>
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<p>The progression of the coefficients for wing lift and F force over five cycles.</p>
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22 pages, 10421 KiB  
Article
Distributed High-Speed Videogrammetry for Real-Time 3D Displacement Monitoring of Large Structure on Shaking Table
by Haibo Shi, Peng Chen, Xianglei Liu, Zhonghua Hong, Zhen Ye, Yi Gao, Ziqi Liu and Xiaohua Tong
Remote Sens. 2024, 16(23), 4345; https://doi.org/10.3390/rs16234345 - 21 Nov 2024
Viewed by 517
Abstract
The accurate and timely acquisition of high-frequency three-dimensional (3D) displacement responses of large structures is crucial for evaluating their condition during seismic excitation on shaking tables. This paper presents a distributed high-speed videogrammetric method designed to rapidly measure the 3D displacement of large [...] Read more.
The accurate and timely acquisition of high-frequency three-dimensional (3D) displacement responses of large structures is crucial for evaluating their condition during seismic excitation on shaking tables. This paper presents a distributed high-speed videogrammetric method designed to rapidly measure the 3D displacement of large shaking table structures at high sampling frequencies. The method uses non-coded circular targets affixed to key points on the structure and an automatic correspondence approach to efficiently estimate the extrinsic parameters of multiple cameras with large fields of view. This process eliminates the need for large calibration boards or manual visual adjustments. A distributed computation and reconstruction strategy, employing the alternating direction method of multipliers, enables the global reconstruction of time-sequenced 3D coordinates for all points of interest across multiple devices simultaneously. The accuracy and efficiency of this method were validated through comparisons with total stations, contact sensors, and conventional approaches in shaking table tests involving large structures with RCBs. Additionally, the proposed method demonstrated a speed increase of at least six times compared to the advanced commercial photogrammetric software. It could acquire 3D displacement responses of large structures at high sampling frequencies in real time without requiring a high-performance computing cluster. Full article
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Graphical abstract

Graphical abstract
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<p>Framework of the proposed videogrammetric method.</p>
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<p>General distributed videogrammetric network.</p>
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<p>Stereo-matching method of circular targets in large FOV (red dots indicate SIFT feature points of stereo images).</p>
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<p>Distributed computation and reconstruction strategy.</p>
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<p>(<b>a</b>) Real structure model. (<b>b</b>) Camera layout and spatial coordinate system. (<b>c</b>) Measurement point distribution.</p>
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<p>Measurement errors between the videogrammetry and the total station at each checkpoint in the X, Y, and Z directions.</p>
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<p>Three-dimensional positioning errors of the checkpoint calculated using different methods after each seismic wave load.</p>
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<p>Comparison of displacement and acceleration response histories obtained by the proposed videogrammetry and contact sensors at points <span class="html-italic">R</span><sub>3</sub> and <span class="html-italic">R</span><sub>18</sub> subjected to different seismic excitations: (<b>a</b>) Experiment No. 1; (<b>b</b>) Experiment No. 3; (<b>c</b>) Experiment No. 5.</p>
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<p>Time consumption and mean reprojection error of different methods for reconstructing the shaking table dataset.</p>
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<p>Time consumption of different methods for reconstructing the shaking table dataset.</p>
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<p>Three-dimensional displacement response histories of measurement points distributed across the coupling beams during (<b>a</b>) Experiment No. 1, (<b>b</b>) Experiment No. 3, and (<b>c</b>) Experiment No. 5.</p>
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22 pages, 5336 KiB  
Review
A Review of the Measurement of the Multiphase Slug Frequency
by Ronaldo Luís Höhn, Abderraouf Arabi, Youssef Stiriba and Jordi Pallares
Processes 2024, 12(11), 2500; https://doi.org/10.3390/pr12112500 - 11 Nov 2024
Viewed by 669
Abstract
The slug frequency (SF), which refers to the number of liquid slugs passing through a pipe during a specific time, is an important parameter for characterizing the multiphase intermittent flows and monitoring some process involving this kind of flow. The simplicity of the [...] Read more.
The slug frequency (SF), which refers to the number of liquid slugs passing through a pipe during a specific time, is an important parameter for characterizing the multiphase intermittent flows and monitoring some process involving this kind of flow. The simplicity of the definition of SF contrasts with the difficulty of correctly measuring it. This manuscript aims to review and discuss the various techniques and methods developed to determine the slug frequency experimentally. This review significantly reveals the absence of a universal measurement method applicable to a wide range of operating conditions. Thus, the recourse to recording videos with high-speed cameras, which can be used only at a laboratory scale, remains often necessary. From the summarized state-of-the-art, it appears that correctly defining the threshold values for detecting the liquid slugs/elongated bubbles interface from physical parameters time series, increasing the applicability of instrumentations at industrial scales, and properly estimating the uncertainties are the challenges that have to be faced to advance in the measurement of SF. Full article
(This article belongs to the Section Energy Systems)
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<p>Schematic presentation of the slug flow for different pipe inclination range. The intrinsic slug parameters are also displayed. Reprinted from [<a href="#B8-processes-12-02500" class="html-bibr">8</a>]. Reprinted from <span class="html-italic">Flow Measurement and Instrumentation</span>, vol. 72, O. Cazarez-Candia, O.C. Benítez-Centeno, Comprehensive experimental study of liquid-slug length and Taylor-bubble velocity in slug flow, page 2, Copyright © 2020, with permission from Elsevier.</p>
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<p>Schematic diagram of the content discussed in the present review.</p>
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<p>Example of illumination system used for camera video recordings used by Mohmmed et al. [<a href="#B22-processes-12-02500" class="html-bibr">22</a>]. Reprinted from <span class="html-italic">International Journal of Pressure Vessels and Piping</span>, vol. 172, Abdalellah O. Mohmmed, Hussain H. Al-Kayiem, Mohammad S. Nasif, Rune W. Time, Effect of slug flow frequency on the mechanical stress behavior of pipelines, page 3, Copyright © 2019, with permission from Elsevier.</p>
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<p>Elongated bubble location using LSI method (air–water, 30 mm ID, <span class="html-italic">θ</span> = 0°, <span class="html-italic">V<sub>SL</sub></span> = 1.5 m/s and <span class="html-italic">V<sub>SG</sub></span> = 0.58 m/s). Reprinted from Sassi et al. [<a href="#B18-processes-12-02500" class="html-bibr">18</a>]. Copyright © 2022, Paulo Sassi et al.</p>
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<p>Example of void fraction time series collected by Maldonado et al. [<a href="#B34-processes-12-02500" class="html-bibr">34</a>] using a capacitive wire-mesh sensor showing the region of Taylor bubble and liquid slug. Reprinted from <span class="html-italic">Experimental Thermal and Fluid Science</span>, vol. 151, Paul A. D. Maldonado, Carolina C. Rodrigues, Ernesto Mancilla, Eduardo N. dos Santos, Roberto da Fonseca Junior, Moises A. Marcelino Neto, Marco J. da Silva, Rigoberto E. M. Morales, Spatial distribution of void fraction in the liquid slug in vertical Gas-Liquid slug flow, page 5, Copyright © 2023, with permission from Elsevier.</p>
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<p>Examples of (<b>a</b>) conductance probe; (<b>b</b>) ECT; (<b>c</b>) WMS used in Zhao et al. [<a href="#B86-processes-12-02500" class="html-bibr">86</a>] (Copyright ©2016, Zhao et al.); and (<b>d</b>) wrapped fiber cable of distributed acoustic sensing (DAS) used by Ali et al. [<a href="#B8-processes-12-02500" class="html-bibr">8</a>] (Copyright ©2024, Ali et al.).</p>
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<p>Example of pressure drop time series showing the peaks induced by the passage of liquid slugs (orange crosses) and by the presence of different kinds of flow structures (waves, roll waves or pseudo slugs) (green crosses). Copyright ©2022, Sassi et al. Note that the green crosses are added and not part of the original source.</p>
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<p>Experimental holdup time series with depiction of the threshold to detect the passage of liquid slugs. Reproduced from Eyo and Lao [<a href="#B124-processes-12-02500" class="html-bibr">124</a>]. Reprinted from <span class="html-italic">AICHE Journal</span>, vol. 65, e16711, Edem N. Eyo, Liyun Lao, Slug flow characterization in horizontal annulus, page 5, Copyright © 2019 American Institute of Chemical Engineers, with permission from WILEY.</p>
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<p>Threshold cut value applied to a normalized voltage or an instantaneous liquid holdup time series. (<b>a</b>) using a single threshold value (<span class="html-italic">TV</span>) and (<b>b</b>) using one threshold value for slug region (<span class="html-italic">TV<sub>slug</sub></span>) and the other for the film (<span class="html-italic">TV<sub>film</sub></span>). Reprinted from <span class="html-italic">Flow Measurement and Instrumentation</span>, vol. 79, Gabriel Soto-Cortes, Eduardo Pereyra, Cem Sarica, Carlos Torres, Auzan Soedarmo, Signal processing for slug flow analysis via a voltage or instantaneous liquid holdup time series, page 2, Copyright © 2021, with permission from Elsevier.</p>
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<p>Example of binarized liquid holdup signals showing the translational times of liquid slug (<span class="html-italic">T<sub>ls</sub></span>) and elongated bubble (<span class="html-italic">T<sub>eb</sub></span>).</p>
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<p>Example of frequency spectrum obtained by applying PSD to the void fraction time series. Taken from [<a href="#B141-processes-12-02500" class="html-bibr">141</a>]. Reprinted from <span class="html-italic">International Journal of Multiphase Flow</span>, vol. 37 (8), Wael H. Ahmed, Experimental investigation of air–oil slug flow using capacitance probes, hot-film anemometer, and image processing, page 886, Copyright © 2011, with permission from Elsevier.</p>
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<p>Comparison between the measured slug frequency using W&amp;M method applied for two pressure tap distances and LSI method obtained by Sassi et al. [<a href="#B17-processes-12-02500" class="html-bibr">17</a>]. Copyright © 2022, Paulo Sassi et al.</p>
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14 pages, 4716 KiB  
Article
Development of a DualEmission Laser-Induced Fluorescence (DELIF) Method for Long-Term Temperature Measurements
by Koji Toriyama, Shumpei Funatani and Shigeru Tada
Sensors 2024, 24(22), 7136; https://doi.org/10.3390/s24227136 - 6 Nov 2024
Viewed by 552
Abstract
The fluorescence intensity of fluorescent dyes typically employed in the dual-emission laser-induced fluorescence (DELIF) method gradually degrades as the excitation time increases, and the degradation rate depends on the type of fluorescent dye used. Therefore, the DELIF method is unsuitable for long-term temperature [...] Read more.
The fluorescence intensity of fluorescent dyes typically employed in the dual-emission laser-induced fluorescence (DELIF) method gradually degrades as the excitation time increases, and the degradation rate depends on the type of fluorescent dye used. Therefore, the DELIF method is unsuitable for long-term temperature measurements. In this study, we focused on the fluorescence intensity ratio of a single fluorescent dye at two fluorescence wavelengths and developed a DELIF method for long-term temperature measurements based on this ratio. The fluorescence intensity characteristics of Fluorescein disodium and Rhodamine B, which are typically used in the DELIF method, in the temperature range of 10–60 °C were comprehensively investigated using two high-speed monochrome complementary metal-oxide semiconductor cameras and narrow bandpass filters. Interestingly, the ratio of the fluorescence intensity of each fluorescent dye at the peak emission wavelength of the fluorescence spectrum, λ, to the fluorescence intensity at wavelengths very close to the peak wavelength (λ ± 10 nm) was highly sensitive to temperature variations but not excitation time. Particularly, when Rhodamine B was used, the selection of the fluorescence intensity ratios at a wavelength combination of 589 and 600 nm enabled highly accurate temperature measurements with a temperature resolution of ≤0.042 °C. Moreover, the fluorescence intensity ratio varied negligibly throughout the excitation time of 180 min, with a measurement uncertainty (95% confidence interval) of 0.045 °C at 20 °C. The results demonstrate that the proposed DELIF method enables highly accurate long-term temperature measurements. Full article
(This article belongs to the Collection Recent Advances in Fluorescent Sensors)
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<p>Experimental setup for fluorescence intensity measurements.</p>
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<p>Fluorescence intensity variations of Rhodamine B, <math display="inline"><semantics> <mrow> <mi>I</mi> <mo>/</mo> <msub> <mrow> <mi>I</mi> </mrow> <mrow> <mi>t</mi> <mo>=</mo> <mn>0</mn> </mrow> </msub> </mrow> </semantics></math>, with excitation time <math display="inline"><semantics> <mrow> <mi>t</mi> </mrow> </semantics></math> at <math display="inline"><semantics> <mrow> <mi>T</mi> <mo>=</mo> <mn>20</mn> </mrow> </semantics></math> °C.</p>
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<p>Experimental setup for fluorescence intensity variation measurements of Fluorescence disodium and Rhodamine B at temperature <math display="inline"><semantics> <mrow> <mi>T</mi> </mrow> </semantics></math>.</p>
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<p>Relationship between the wavelength <math display="inline"><semantics> <mrow> <mi>λ</mi> </mrow> </semantics></math> and fluorescence intensity at various temperatures <math display="inline"><semantics> <mrow> <mi>T</mi> </mrow> </semantics></math>, for (<b>a</b>,<b>b</b>).</p>
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<p>Relationship between the temperature and fluorescence intensity ratios of Fluorescein disodium for wavelength combinations of 500/510 nm and 520/510 nm and of Rhodamine B for wavelength combinations of 580/589 nm and 600/589 nm obtained using a spectrometer.</p>
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<p>Experimental setup for the DELIF method with one dye. Two cameras and bandpass filters were used in this experiment.</p>
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<p>(<b>a</b>) Relationship between the temperature and fluorescence intensity and, (<b>b</b>) Relationship between the temperature and rate of fluorescence intensity variation with temperature, at different emission wavelengths for Fluorescein disodium (<math display="inline"><semantics> <mrow> <mi>λ</mi> <mo> </mo> </mrow> </semantics></math> = 500, 510, and 520 nm) and Rhodamine B (<math display="inline"><semantics> <mrow> <mi>λ</mi> </mrow> </semantics></math> = 580, 589, and 600 nm).</p>
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<p>Relationship between the temperature and fluorescence intensity ratios of Fluorescein disodium for wavelength combinations of 500/510 nm and 520/510 nm and of Rhodamine B for wavelength combinations of 580/589 nm and 600/589 nm obtained using CMOS cameras and bandpass filters.</p>
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<p>Relationships between the temperature and temperature resolutions of Fluorescein disodium for wavelength combinations of 500 and 510 nm and 520 and 510 nm, and of Rhodamine B for wavelength combinations of 580 and 589 nm and 600 and 589 nm.</p>
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<p>Relationships between the excitation time and fluorescence intensity ratios at 20 °C Fluorescein disodium for wavelength combinations of 500 and 510 nm and 520 and 510 nm, and of Rhodamine B for wavelength combinations of 580 and 589 nm and 600 and 589 nm.</p>
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13 pages, 5756 KiB  
Technical Note
Machine Learning Based Peach Leaf Temperature Prediction Model for Measuring Water Stress
by Heetae Kim, Minyoung Kim, Youngjin Kim, Byounggap Kim, Choungkeun Lee and Jaeseung No
Water 2024, 16(21), 3157; https://doi.org/10.3390/w16213157 - 4 Nov 2024
Viewed by 836
Abstract
When utilizing the Crop Water Stress Index (CWSI), the most critical factor is accurately measuring canopy temperature, which is typically done using infrared sensors and imaging cameras. In this study, however, we aimed to develop a machine learning model capable of predicting leaf [...] Read more.
When utilizing the Crop Water Stress Index (CWSI), the most critical factor is accurately measuring canopy temperature, which is typically done using infrared sensors and imaging cameras. In this study, however, we aimed to develop a machine learning model capable of predicting leaf temperature based on environmental data, without relying on sensors, for calculating CWSI. The data underwent preprocessing to remove outliers and missing values. The number of training data points for each factor was 307,924. After data preprocessing, a Pearson correlation analysis (bivariate correlation coefficient) was conducted to select the training data for model operation. The relationship between leaf temperature and air temperature showed a strong positive correlation of 0.928 (p < 0.01). Solar radiation and relative humidity were also found to have high correlations. However, wind speed and soil moisture tension showed very low correlations with leaf temperature and were excluded from the model operation. The Decision Tree, Random Forest, and Gradient Boosting models were selected, and each model was evaluated using RMSE (Root Mean Squared Error), MAE (Mean Absolute Error), MSE (Mean Squared Error), and R2 (coefficient of determination). The evaluation results showed that the Gradient Boosting model had a high R2 (0.97) and low RMSE (0.88) and MAE (0.54), making it the most suitable model for predicting leaf temperature. Through the leaf temperature prediction model developed in this study, labor and costs associated with sensors can be reduced, and by applying it to real agricultural settings, it can improve crop quality and enhance the sustainability of agriculture. Full article
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<p>Experimental site(Peach orchard) for data measurement. (Purple Box: latitude 35°49′29″; longitude 127°01′32″; scale 2475 m<sup>2</sup>).</p>
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<p>Schematic diagram of the DT model (nodes and leaves are colored green and brown, respectively) [<a href="#B27-water-16-03157" class="html-bibr">27</a>].</p>
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<p>Schematic diagram of RF classifier (nodes and leaves are colored green and brown, respectively) [<a href="#B27-water-16-03157" class="html-bibr">27</a>].</p>
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<p>Schematic diagram of GBM classifier(nodes and leaves are colored green and brown, respectively) [<a href="#B27-water-16-03157" class="html-bibr">27</a>].</p>
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<p>Monthly comparison of observed and predicted leaf temperature values for June 2020.</p>
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<p>Monthly comparison of observed and predicted leaf temperature values for July 2020.</p>
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<p>Monthly comparison of observed and predicted leaf temperature values for August 2020.</p>
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<p>Monthly comparison of observed and predicted leaf temperature values for September 2020.</p>
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<p>Monthly comparison of observed and predicted leaf temperature values for June 2022.</p>
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<p>Monthly comparison of observed and predicted leaf temperature values for July 2022.</p>
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<p>Monthly comparison of observed and predicted leaf temperature values for August 2022.</p>
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<p>Monthly comparison of observed and predicted leaf temperature values for September 2022.</p>
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<p>Box plot of the GBM (Green triangle: Mean value of the data).</p>
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36 pages, 37451 KiB  
Review
Non-Spherical Cavitation Bubbles: A Review
by Boxin Jia and Hitoshi Soyama
Fluids 2024, 9(11), 249; https://doi.org/10.3390/fluids9110249 - 25 Oct 2024
Viewed by 1314
Abstract
Cavitation is a phase-change phenomenon from the liquid to the gas phase due to an increased flow velocity. As it causes severe erosion and noise, it is harmful to hydraulic machinery such as pumps, valves, and screw propellers. However, it can be utilized [...] Read more.
Cavitation is a phase-change phenomenon from the liquid to the gas phase due to an increased flow velocity. As it causes severe erosion and noise, it is harmful to hydraulic machinery such as pumps, valves, and screw propellers. However, it can be utilized for water treatment, in chemical reactors, and as a mechanical surface treatment, as radicals and impacts at the point of cavitation bubble collapse can be utilized. Mechanical surface treatment using cavitation impacts is called “cavitation peening”. Cavitation peening causes less pollution because it uses water to treat the mechanical surface. In addition, cavitation peening improves on traditional methods in terms of fatigue strength and the working life of parts in the automobile, aerospace, and medical fields. As cavitation bubbles are utilized in cavitation peening, the study of cavitation bubbles has significant value in improving this new technique. To achieve this, many numerical analyses combined with field experiments have been carried out to measure the stress caused by bubble collapse and rebound, especially when collapse occurs near a solid boundary. Understanding the mechanics of bubble collapse can help to avoid unnecessary surface damage, enabling more accurate surface preparation, and improving the stability of cavitation peening. The present study introduces three cavitation bubble types: single, cloud, and vortex cavitation bubbles. In addition, the critical parameters, governing equations, and high-speed camera images of these three cavitation bubble types are introduced to support a broader understanding of the collapse mechanism and characteristics of cavitation bubbles. Then, the results of the numerical and experimental analyses of non-spherical cavitation bubbles are summarized. Full article
(This article belongs to the Special Issue Cavitation and Bubble Dynamics)
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<p>Improvement in the fatigue strength of the test gear via cavitation peening. Reprint from [<a href="#B35-fluids-09-00249" class="html-bibr">35</a>], with permission from Taylor and Francis, 2009, License Number 5803511487624.</p>
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<p>Images of laser cavitation on the wall near the glass chamber [<a href="#B56-fluids-09-00249" class="html-bibr">56</a>].</p>
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<p>Collapse of a solid cavitation bubble near a boundary in water, computed by Plesset and Chapman. A–I represent different shapes as time goes on. Reprint from [<a href="#B49-fluids-09-00249" class="html-bibr">49</a>], with permission from Cambridge University Press, 1971, License Number 5724030138904.</p>
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<p>Cavitation bubble dynamics in the vicinity of a solid boundary. Reprint from [<a href="#B11-fluids-09-00249" class="html-bibr">11</a>], with permission from Cambridge University Press, 1998, License Number 5831440015629.</p>
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<p>Growth of cavity from nucleus very close to a solid wall, and subsequent collapse. Timing: (<b>A</b>–<b>C</b>) at 0, 0.2, and 0.4; (<b>D</b>–<b>F</b>) at 5.8, 6.0, and 6.2; (<b>G</b>–<b>I</b>) at 11.4, 11.6, and 11.8; (<b>J</b>–<b>O</b>) at 16.8 to 17.8 ms. Reprint from [<a href="#B48-fluids-09-00249" class="html-bibr">48</a>], with permission from Royal Society (Great Britain), 1966, License Number 1492359-1.</p>
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<p>The bubble–wall Mach number as a function of the bubble radius with a decreasing gas content. The gas content is determined by its initial pressure <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>p</mi> </mrow> <mrow> <mn>0</mn> </mrow> </msub> </mrow> </semantics></math> in atmospheres. The index <math display="inline"><semantics> <mrow> <mi>γ</mi> </mrow> </semantics></math> has the value 1.4, and the ambient pressure <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>p</mi> </mrow> <mrow> <mo>∞</mo> </mrow> </msub> </mrow> </semantics></math> is 1 atm. Reprint from [<a href="#B47-fluids-09-00249" class="html-bibr">47</a>], with permission from AIP Publishing, 1964, License Number 5806350103845.</p>
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<p>Water hammer shock in free-field shock-induced collapse (<math display="inline"><semantics> <mrow> <msub> <mrow> <mi>p</mi> </mrow> <mrow> <mi>s</mi> </mrow> </msub> </mrow> </semantics></math>/<math display="inline"><semantics> <mrow> <msub> <mrow> <mi>p</mi> </mrow> <mrow> <mi>o</mi> </mrow> </msub> </mrow> </semantics></math> = 353) at times (<b>a</b>) <math display="inline"><semantics> <mrow> <mi>t</mi> <mo>/</mo> <mo>(</mo> <msub> <mrow> <mi>R</mi> </mrow> <mrow> <mi>o</mi> </mrow> </msub> <mo>/</mo> <msub> <mrow> <mi>c</mi> </mrow> <mrow> <mi>L</mi> </mrow> </msub> </mrow> </semantics></math>) = 8.49, (<b>b</b>) <math display="inline"><semantics> <mrow> <mi>t</mi> <mo>/</mo> <mo>(</mo> <msub> <mrow> <mi>R</mi> </mrow> <mrow> <mi>o</mi> </mrow> </msub> <mo>/</mo> <msub> <mrow> <mi>c</mi> </mrow> <mrow> <mi>L</mi> </mrow> </msub> </mrow> </semantics></math>) == 8.68, (<b>c</b>) <math display="inline"><semantics> <mrow> <mi>t</mi> <mo>/</mo> <mo>(</mo> <msub> <mrow> <mi>R</mi> </mrow> <mrow> <mi>o</mi> </mrow> </msub> <mo>/</mo> <msub> <mrow> <mi>c</mi> </mrow> <mrow> <mi>L</mi> </mrow> </msub> </mrow> </semantics></math>) == 9.05, (<b>d</b>) <math display="inline"><semantics> <mrow> <mi>t</mi> <mo>/</mo> <mo>(</mo> <msub> <mrow> <mi>R</mi> </mrow> <mrow> <mi>o</mi> </mrow> </msub> <mo>/</mo> <msub> <mrow> <mi>c</mi> </mrow> <mrow> <mi>L</mi> </mrow> </msub> </mrow> </semantics></math>) == 9.52. Top: density lines; bottom: pressure contours non-dimensionalized by <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>ρ</mi> </mrow> <mrow> <mi>L</mi> </mrow> </msub> <msubsup> <mrow> <mi>c</mi> </mrow> <mrow> <mi>L</mi> </mrow> <mrow> <mn>2</mn> </mrow> </msubsup> </mrow> </semantics></math> (approximate interface location: γ = 1.42 contour). <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>p</mi> </mrow> <mrow> <mi>s</mi> </mrow> </msub> </mrow> </semantics></math>: The shock pressure; <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>p</mi> </mrow> <mrow> <mi>o</mi> </mrow> </msub> </mrow> </semantics></math>: The relevant pressure ahead of the compression;<math display="inline"><semantics> <mrow> <mtext> </mtext> <msub> <mrow> <mi>R</mi> </mrow> <mrow> <mi>o</mi> </mrow> </msub> </mrow> </semantics></math>: The radius of bubble; <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>ρ</mi> </mrow> <mrow> <mi>L</mi> </mrow> </msub> </mrow> </semantics></math>: The ambient density of the water; <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>c</mi> </mrow> <mrow> <mi>L</mi> </mrow> </msub> </mrow> </semantics></math>: The sound speed of the water. Reprint from [<a href="#B52-fluids-09-00249" class="html-bibr">52</a>], with permission from Cambridge University Press, 2009, License Number 5830760763951.</p>
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<p>The final stage of the collapse of a cavitation bubble for <math display="inline"><semantics> <mrow> <mi>γ</mi> <mo>=</mo> <mn>1.1</mn> </mrow> </semantics></math>. (<b>a</b>) High-speed photographic record of bubble motion; frame interval 200 ns, frame width 1.4 mm. The location of the rigid boundary is at the upper limit of the frames. (<b>b</b>) Computed bubble profiles covering the time interval correspond to the photographic record’s first row. The nondimensional times are t = 2.0084, 2.0097, 2.011, 2.0123, 2.0136, 2.0149, 2.0161, 2.0174, 2.0187, 2.02, and 2.0213. Reprint from [<a href="#B50-fluids-09-00249" class="html-bibr">50</a>], with permission from AIP Publishing, 2002, License Number 5806350497331.</p>
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<p>Evolution of the velocity field (<b>right</b>) and pressure contours (<b>left</b>) for the toroidal stage of bubble collapse for <math display="inline"><semantics> <mrow> <mi>γ</mi> </mrow> </semantics></math> = 1.1. The letters correspond to the following nondimensional times: (<b>a</b>) 1.9981, (<b>b</b>) 2.011, and (<b>c</b>) 2.0213. Reprint from [<a href="#B50-fluids-09-00249" class="html-bibr">50</a>], with permission from AIP Publishing, 2002, License Number 5806350497331.</p>
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<p>Time variation in pressure in fluid and equivalent stress in material on wet surface. Reprint from [<a href="#B60-fluids-09-00249" class="html-bibr">60</a>], with permission from J-stage, 2016.</p>
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<p>The mathematical model of the non-spherical bubble [<a href="#B45-fluids-09-00249" class="html-bibr">45</a>].</p>
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<p>Time evolution of the void fraction (<b>upper left</b> of each sub-figure), pressure, and velocity vectors (<b>upper right</b>) in the fluid domain, and equivalent stress in the material domain (<b>lower</b>) (<math display="inline"><semantics> <mrow> <mi>γ</mi> <mo>=</mo> </mrow> </semantics></math> 0.5) [<a href="#B45-fluids-09-00249" class="html-bibr">45</a>].</p>
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<p>Variation in maximum equivalent stress and stress influence area with the stand-off distance between the bubble and the wall. The blue and red arrows point <math display="inline"><semantics> <mrow> <mi>γ</mi> <mo>/</mo> <msub> <mrow> <mi>R</mi> </mrow> <mrow> <mn>0</mn> </mrow> </msub> </mrow> </semantics></math> = 1 and 0.5. [<a href="#B45-fluids-09-00249" class="html-bibr">45</a>].</p>
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<p>Evolution of the axial section of a bubble collapsing near a plane wall (<math display="inline"><semantics> <mrow> <msub> <mrow> <mi mathvariant="normal">t</mi> </mrow> <mrow> <mn>0</mn> </mrow> </msub> </mrow> </semantics></math> corresponds to the beginning of collapse): (<b>a</b>) the results of a simulation of the interaction between two bubbles by the proposed model (solid lines correspond to the bubble under consideration; dashed lines present its mirror image), and (<b>b</b>) the same results for the bubble considered (solid lines), along with experimental data and the results obtained by the boundary element method (dashed lines). Reprint from [<a href="#B61-fluids-09-00249" class="html-bibr">61</a>], with permission from Elsevier, 2024, License Number 5830790844530.</p>
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<p>Interaction between three bubbles simultaneously produced collinearly at nearly equal inter-bubble distances: (<b>a</b>) in the experiments by Cui et al., and (<b>b</b>) in the simulation by the present model. Reprint from [<a href="#B61-fluids-09-00249" class="html-bibr">61</a>], with permission from Elsevier, 2024, License Number 5830790844530.</p>
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<p>Consecutive high-speed movie frames (2 ms apart) showing global cloud collapse. (<b>a</b>–<b>d</b>) depict four consecutive frames from one such movie. Reprint from [<a href="#B63-fluids-09-00249" class="html-bibr">63</a>], with permission from Cambridge University Press, 1998, License Number 5830810037327.</p>
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<p>Collapse phase of a hemispherical bubble cloud. Frame interval 500 ns. The first frame was taken 159.55 <math display="inline"><semantics> <mrow> <mi mathvariant="sans-serif">μ</mi> <mi mathvariant="normal">s</mi> </mrow> </semantics></math> after the application of ultrasound. Frame width 2.56 mm. The collapse point of the cloud occurs between frames 7 and 8. The main shock wave emission during cloud rebound can be seen in frames 8 and 9. Reprint from [<a href="#B51-fluids-09-00249" class="html-bibr">51</a>], with permission from Elsevier, 2011, License Number 5830811192279.</p>
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<p>Comparison of bubble radii at different cloud locations for a bubble cloud excited at different pressure frequencies: (<b>a</b>) f = 25 kHz; (<b>b</b>) f = 8 kHz, and (<b>c</b>) f = 5 kHz [<a href="#B65-fluids-09-00249" class="html-bibr">65</a>].</p>
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<p>The mathematical model of cloud bubbles [<a href="#B66-fluids-09-00249" class="html-bibr">66</a>], with permission from Elsevier, 2018, License Number 5880601502087.</p>
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<p>Time sequence of bubble distributions and internal pressures (indicated by the colored contours) in a bubble cloud driven by pressure excitation with two amplitudes. The last frame of each row is a view of the pressures at the rigid wall [<a href="#B66-fluids-09-00249" class="html-bibr">66</a>], with permission from Elsevier, 2018, License Number 5880601502087.</p>
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<p>Strong interaction between the bubble and sphere near a rigid boundary. (<b>a</b>) Experimental images. Frames 1–9 depict the first cycle of the bubble and it is noted that the bubble bottom gains a higher local curvature (frames 4–6) due to the retardation effect from the sphere. An upward jet forms at the bubble bottom afterwards, and a strong spray at the jet tip can be observed in frame 7, leading to the unstable bubble surface after the jet impact. Frames 10–14 depict the second cycle of the bubble. The bubble migrates towards the wall during the rebounding phase and collapses onto the wall directly in the recollapse phase (frames 13 and 14). (<b>b</b>) Numerical results. The jet tip assumes a mushroom shape, which has favorable agreement with the experiment. Reprint from [<a href="#B53-fluids-09-00249" class="html-bibr">53</a>], with permission from AIP Publishing, 2017, License Number 5830821246785.</p>
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<p>Time evolution of bubble radius and void fraction distribution for various stand-off distances. Reprint from [<a href="#B67-fluids-09-00249" class="html-bibr">67</a>], with permission from Elsevier, 2022, License Number 5830830883340.</p>
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<p>Snapshots of cloud cavitation in four successive shedding cycles. Reprint from [<a href="#B68-fluids-09-00249" class="html-bibr">68</a>] with permission from AIP Publishing, 2023, License Number 5830840703844.</p>
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<p>Observed and predicted time evolution of the multi-scale cavitating flow around the twisted hydrofoil: (<b>a</b>) experimental pictures, (<b>b</b>) global simulation results, and (<b>c</b>) partially enlarged simulation results. Reprint from [<a href="#B70-fluids-09-00249" class="html-bibr">70</a>], with permission from Elsevier, 2023, License Number 5830841056536.</p>
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<p>(<b>a</b>) Typical cavitating flow fields and (<b>b</b>) probability density of discrete bubble numbers at two typical instants during stage I. Reprint from [<a href="#B70-fluids-09-00249" class="html-bibr">70</a>], with permission from Elsevier, 2023, License Number 5830841056536.</p>
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<p>Typical vortex cavitation [<a href="#B71-fluids-09-00249" class="html-bibr">71</a>].</p>
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<p>Photographs showing the development of a tip and other forms of cavitation on a hydrofoil, showing the continuous tip vortex cavity, tip vortex cavitation, secondary vortex cavitation, and surface cavitation. Reprint from [<a href="#B72-fluids-09-00249" class="html-bibr">72</a>], with permission from Cambridge University Press, 1991, License Number 5860660245448.</p>
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<p>Top view of cavity shedding patterns for <math display="inline"><semantics> <mrow> <mi>σ</mi> <mo>=</mo> <mn>1.07</mn> </mrow> </semantics></math> during one typical cycle (<b>a</b>–<b>g</b>). (Left: numerical results. Right: experimental observation by Foeth (2008) [<a href="#B74-fluids-09-00249" class="html-bibr">74</a>].) Reprint from [<a href="#B73-fluids-09-00249" class="html-bibr">73</a>] with permission from Elsevier, 2014, License Number 5830860095566.</p>
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<p>Comparison of vapor volume fraction (<b>left</b>) and vorticity (<b>right</b>) contours for <math display="inline"><semantics> <mrow> <mi>σ</mi> <mo>=</mo> <mn>1.07</mn> </mrow> </semantics></math> at the plane with <math display="inline"><semantics> <mrow> <mi>z</mi> <mo>=</mo> <mn>0</mn> </mrow> </semantics></math> during one typical cycle (<b>a</b>–<b>g</b>). Reprint from [<a href="#B73-fluids-09-00249" class="html-bibr">73</a>] with permission from Elsevier, 2014, License Number 5830860095566.</p>
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<p>Schematic drawing of JPCR [<a href="#B29-fluids-09-00249" class="html-bibr">29</a>].</p>
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<p>Typical cavitation images at the minimum outlet pressure for different JPCRs [<a href="#B29-fluids-09-00249" class="html-bibr">29</a>].</p>
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<p>Typical cavitation images at the minimum outlet pressure for JPCRs with different structures [<a href="#B29-fluids-09-00249" class="html-bibr">29</a>].</p>
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<p>Measured cavitation results with a vortex generator within a typical cycle. Reprint from [<a href="#B75-fluids-09-00249" class="html-bibr">75</a>] with permission from Elsevier, 2020, License Number 5831390551079.</p>
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<p>Typical aspects of cavitation in a Venturi tube: (<b>a</b>) aspects changing with downstream pressure p2 (p1 = 0.6 MPa); (<b>b</b>) aspect changing with upstream pressure p1 (p2 = 0.1 MPa) [<a href="#B28-fluids-09-00249" class="html-bibr">28</a>].</p>
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<p>Relationship between measured luminescence intensity and estimated luminescence intensity [<a href="#B28-fluids-09-00249" class="html-bibr">28</a>].</p>
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<p>Numerical and experimental study on the behavior of vortex rings generated by shock–bubble interaction. (<b>a</b>) two–dimensional views; (<b>b</b>) three–dimensional views; (<b>c</b>) vorticity contours at t=16 μs. Reprint from [<a href="#B77-fluids-09-00249" class="html-bibr">77</a>], with permission from AIP Publishing, 2022, License Number 5831411280013.</p>
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<p>One-cycle shedding process of the cloud cavitation. A: horse-type cavity structure; B: small-scale U-type vortex; C: re-entrant jet; D: vortex tubes; E: non-uniform distribution of cavity and re-entrant jet. The cavity is visualized by the iso-surface with a vapor fraction of 0.1. All the structures are colored in terms of the spanwise vorticity component. Reprint from [<a href="#B78-fluids-09-00249" class="html-bibr">78</a>], with permission from Springer Nature, 2022, License Number 5831420313482.</p>
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<p>Cross-section of the velocity field with represented volume fraction contour <math display="inline"><semantics> <mrow> <mi>γ</mi> <mo>=</mo> <mn>0.1</mn> </mrow> </semantics></math> [<a href="#B80-fluids-09-00249" class="html-bibr">80</a>].</p>
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<p>Bubble evolution for <math display="inline"><semantics> <mrow> <msub> <mrow> <mi>p</mi> </mrow> <mrow> <mi>i</mi> <mi>n</mi> </mrow> </msub> <mo>=</mo> <mn>3</mn> <mo>–</mo> <mn>6</mn> </mrow> </semantics></math> bar [<a href="#B80-fluids-09-00249" class="html-bibr">80</a>].</p>
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<p>Comparison of nondimensional velocity distribution within the tip vortex region at downstream location <math display="inline"><semantics> <mrow> <mi>x</mi> <mo>/</mo> <msub> <mrow> <mi>c</mi> </mrow> <mrow> <mn>0</mn> </mrow> </msub> <mo>=</mo> <mn>1.14</mn> <mo>,</mo> </mrow> </semantics></math> as obtained from simulations with different mesh sizes, with the experimental measurement [<a href="#B81-fluids-09-00249" class="html-bibr">81</a>].</p>
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<p>Vortex cavitation from shedding of trailing edge to collapse, observed by high-speed X-ray imaging. (<b>a</b>) Standard view of one cycle. (<b>b</b>) Magnified view [<a href="#B55-fluids-09-00249" class="html-bibr">55</a>].</p>
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<p>Vortex cavitation from shedding of trailing edge to collapse, observed by high-speed X-ray imaging. (<b>a</b>) Standard view of one cycle. (<b>b</b>) Magnified view [<a href="#B55-fluids-09-00249" class="html-bibr">55</a>].</p>
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<p>Rotation of vortex cavitation arising in the Venturi tube observed by XFEL [<a href="#B55-fluids-09-00249" class="html-bibr">55</a>].</p>
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24 pages, 9759 KiB  
Article
Experimental and Numerical Evaluation of Calcium-Silicate-Based Mineral Foam for Blast Mitigation
by Aldjabar Aminou, Mohamed Ben Rhouma, Bachir Belkassem, Hamza Ousji, Lincy Pyl and David Lecompte
Appl. Sci. 2024, 14(21), 9656; https://doi.org/10.3390/app14219656 - 22 Oct 2024
Viewed by 698
Abstract
Cellular materials such as aluminum and polyurethane foams are recognized for their effectiveness in energy absorption. They commonly serve as crushable cores in sacrificial cladding for blast mitigation purposes. This study delves into the effectiveness of autoclaved aerated concrete (AAC), a lightweight, porous [...] Read more.
Cellular materials such as aluminum and polyurethane foams are recognized for their effectiveness in energy absorption. They commonly serve as crushable cores in sacrificial cladding for blast mitigation purposes. This study delves into the effectiveness of autoclaved aerated concrete (AAC), a lightweight, porous material known for its energy-absorbing properties as a crushable core in sacrificial cladding. The experimental set-up features a rigid frame made of steel measuring 1000 × 1000 × 15 mm3 with a central square opening (300 × 300 mm2) holding a 2 mm thick aluminum plate representing the structure. The dynamic response of the aluminum plate is captured using two high-speed cameras arranged in a stereoscopic configuration. Three-dimensional digital image correlation is used to compute the transient deformation fields. Blast loading is achieved by detonating 20 g of C4 explosive set at 250 mm from the plate’s center. The study assesses the mineral foam’s absorption capacity by comparing out-of-plane displacement and mean permanent deformation of the aluminum plate with and without the protective solution. Six foam configurations (A to F) are tested experimentally and numerically, varying in the foam’s free space for expansion relative to its total volume. Results show positive protective effects, with configuration F reducing maximum deflection by at least 30% and configuration C by up to 70%. Foam configuration influences energy dissipation, with an optimal lateral surface-to-volume ratio (ζ) enhancing protective effects, although excessive ζ leads to non-uniform foam crushing. To address the influence of front skin deformability, a non-deformable front skin has been adopted. The latter demonstrates an increased effectiveness of the sacrificial cladding, particularly for ζ values above the optimal value obtained when using a deformable front skin. Notably, using a non-deformable front skin increases maximum deflection reduction and foam energy absorption by up to approximately 30%. Full article
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Figure 1
<p>(<b>a</b>) Overview of the set-up showing the steel frame, two high-speed cameras (Photron Fastcam SA5, Photron, Bucks, UK) arranged stereoscopically, and three LED spots; (<b>b</b>) speckle pattern applied on the aluminum backplate (EN AW-1050 A H24, Thyssenkrupp, Brussels, Belgium) enabling measuring the displacement and in-plane strain fields; and (<b>c</b>) 20 g of C4 explosive charge in a spherical shape and electric detonator.</p>
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<p>Tested samples (<b>a</b>) backplate without foam and (<b>b</b>) backplate with mineral foam of 60 mm thickness and front skin of 2 mm thickness.</p>
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<p>60 mm thick foam in single-volume (<b>a</b>) and spaced foam (<b>b</b>,<b>c</b>) configurations adopted for the experimental tests.</p>
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<p>(<b>a</b>) Thick aluminum plate equipped with four high-pressure transducers; and (<b>b</b>) Schematic of the geometry of aluminum plate specimen.</p>
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<p>Pressure–time histories for 20 g of C4 set at (<b>a</b>) 250 mm and (<b>b</b>) 188 mm.</p>
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<p>Pressure–time histories from Gauge 1 in three different tests to assess the reproducibility of 20 g of C4 set at (<b>a</b>) 250 mm and (<b>b</b>) 188 mm.</p>
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<p>Mean (<b>a</b>) peak pressures and (<b>b</b>) impulses along with their standard deviations with and without the sacrificial cladding.</p>
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<p>Response of the unprotected backplate (<b>a</b>) deflection profiles for test 2 and (<b>b</b>) mid-span deflections.</p>
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<p>Experimental deflection profiles for tests 1: (<b>a</b>) Without the protective foam, (<b>b</b>) in Configuration A, (<b>c</b>) in Configuration B, and (<b>d</b>) in Configuration C.</p>
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<p>Mitigation of the blast load through pulverization of the mineral foam.</p>
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<p>Post-mortem visual inspection of the fractured foam layer for configuration A.</p>
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<p>Mid-span deflection of the backplate with and without the protective foam. Tests 1 are shown with a solid line, Tests 2 with a dotted line and Tests 3 with dash-dot line.</p>
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<p>(<b>a</b>) Front view of the experimental set-up in finite element model and (<b>b</b>) One-quarter of the SC solution with the foam in SPH viewed from the rear of the set-up (front skin in green-foam-backplate in red).</p>
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<p>Convergence study of the mesh size on the aluminum plates and the mineral foam.</p>
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<p>Quasi-static and dynamic compression stress-strain curves that were inserted as a table for the Fu Chang Foam material model.</p>
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<p>Additional configurations adopted for numerical simulation: (<b>a</b>) Configuration D, (<b>b</b>) Configuration E, and (<b>c</b>) Configuration F.</p>
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<p>Comparison of numerical and experimental reflected over-pressure measured by Gauge 1. (<b>a</b>) Results without the protective foam and (<b>b</b>) results with 60 mm thick foam cladding.</p>
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<p>Comparison between the experimental and numerical deflection at the backplate’s center with the protective foam for configuration A.</p>
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<p>Experimental and numerical deflection profiles: (<b>a</b>) Without the protective foam, (<b>b</b>) Configuration A, (<b>c</b>) Configuration B, and (<b>d</b>) Configuration C.</p>
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<p>Bar chart illustrating the maximum deflection of the backplate’s center across various configurations and three charge masses.</p>
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<p>Bar chart illustrating the mean permanent deformation of the backplate’s center across various configurations and three charge masses.</p>
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<p>Maximum deflection at the backplate’s center as a function of ζ and for different explosive charge masses.</p>
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<p>Absorbed energy by the foam as a function of ζ and for different explosive charge masses.</p>
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<p>Isometric view of the out-of-plane displacements (in mm) of the backplate (top plate), foam and front skin of the different configurations.</p>
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<p>Deflection profiles at mid-plane of the backplate and the front skin.</p>
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<p>Foam level of crushing across various foam configurations and a charge mass of 50 g TNT equivalent.</p>
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<p>Evolution up to 0.6 ms in an isometric view of the out-of-plane displacements (in mm) of the backplate (top plate), foam and front skin of the different configurations for configurations C, D, and E.</p>
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<p>Influence of front skin deformability on the maximum deflection at the backplate’s center across various foam configurations.</p>
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<p>Influence of front skin deformability on the absorbed energy by the foam for different foam configurations.</p>
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15 pages, 8216 KiB  
Article
20 kHz CH2O- and SO2-PLIF/OH*-Chemiluminescence Measurements on Blowoff in a Non-Premixed Swirling Flame under Fuel Mass Flow Rate Fluctuations
by Chen Fu, Xiaoyang Wang, Yunhui Wu and Yi Gao
Appl. Sci. 2024, 14(20), 9419; https://doi.org/10.3390/app14209419 - 16 Oct 2024
Viewed by 749
Abstract
Blowoff limits are essential in establishing the combustor operating envelope. Hence, there is a great demand for practical aero-engines to extend the blowoff limits further. In this work, the behavior of non-premixed swirling flames under fuel flow rate oscillations was investigated experimentally close [...] Read more.
Blowoff limits are essential in establishing the combustor operating envelope. Hence, there is a great demand for practical aero-engines to extend the blowoff limits further. In this work, the behavior of non-premixed swirling flames under fuel flow rate oscillations was investigated experimentally close to its blowoff limits. The methane flame was stabilized on the axisymmetric bluff body and confined in a square quartz enclosure. External acoustic forcing at 400 Hz was applied to the fuel flow to induce a fuel mass flow rate fluctuation (FMFRF) with varying amplitudes. A high-speed burst-mode laser and cameras ran at 20 kHz for OH*-chemiluminescence (CL), CH2O-, and SO2-PLIF measurements, offering the visualization of the two-dimensional flame structure and heat release distribution, temporally and spatially. The results show that the effect of FMFRF is predominantly along the central axis without altering the time-averaged flame structure and blowoff transient. However, the blowoff limits are extended due to the enhanced temperature and longer residence time induced by FMFRF. This work allows us to explore the mechanism of flame instability further. Full article
(This article belongs to the Section Aerospace Science and Engineering)
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Figure 1
<p>(<b>a</b>) Schematic of the burner and (<b>b</b>) flame structure of non-premixed swirling flame [<a href="#B59-applsci-14-09419" class="html-bibr">59</a>,<a href="#B60-applsci-14-09419" class="html-bibr">60</a>].</p>
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<p>(<b>a</b>) Axial velocity fluctuation of the fuel at the jet nozzle as a function of the loudspeaker voltage for 5 different mean fuel velocities and (<b>b</b>) time-resolved velocity under a loudspeaker voltage of 0.6 V (FMFRF amplitude ~80%) along the jet centerline at the downstream height of 1 mm above the nozzle exit in three acoustic periods with a time interval of 0.1 ms.</p>
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<p>High-speed PLIF/chemiluminescence imaging system.</p>
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<p>The processes of laser intensity correction. (<b>a</b>) The images of the cuvette, (<b>b</b>) the profile of laser intensity, (<b>c</b>) uncorrected PLIF, and (<b>d</b>) corrected PLIF (CH<sub>2</sub>O-PLIF on the left and SO<sub>2</sub>-PLIF on the right). The sample image is from the flame forced by an 80% FMFRF amplitude at a mean fuel mass flow rate of 0.142 g/s and air velocity of 17.1 m/s.</p>
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<p>The left half of the inverse Abel-transformed time-averaged OH*-CL images with varying FMFRFs (displayed at the top of every image) at the conditions with a mean fuel mass flow rate of 0.142 g/s and air velocity of 17.1 m/s.</p>
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<p>Comparison of time-averaged (<b>a</b>) CH<sub>2</sub>O- and (<b>b</b>) SO<sub>2</sub>-PLIF images at the unforced (left half) and forced cases (right half) with 80% FMFRF amplitude at a mean fuel mass flow rate of 0.142 g/s and air velocity of 17.1 m/s.</p>
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<p>Phase-averaged CH<sub>2</sub>O- (<b>every left</b>) and SO<sub>2</sub>-PLIF (<b>every right</b>) images from flames at a mean fuel mass flow rate of 0.142 g/s and air velocity of 17.1 m/s with 80% FMFRF, and the phase is marked in every subgraph.</p>
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<p>A sequence of instantaneous CH<sub>2</sub>O-PLIF (<b>a</b>,<b>c</b>) and SO<sub>2</sub>-PLIF (<b>b</b>,<b>d</b>) images taken in flames at a mean fuel mass flow rate of 0.142 g/s and air velocity of 17.1 m/s at the unforced (<b>a</b>,<b>b</b>) and forced cases (<b>c</b>,<b>d</b>) with 80% FMFRF. The SO<sub>2</sub>-PLIF signal at <span class="html-italic">z</span> = 18 mm (red dotted line in (<b>b</b>,<b>d</b>)) is presented in (<b>e</b>) to highlight the temperature rise in the shear layer. Note that the CH<sub>2</sub>O- and SO<sub>2</sub>-PLIF were not simultaneous.</p>
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<p>The blowoff air velocity as a function of the varying FMFRF amplitude at a mean fuel mass flow rate of 0.142 g/s.</p>
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<p>Time sequence of instantaneous OH*-CL images during an individual blowoff event at a mean fuel mass flow rate of 0.142 g/s with no acoustic forcing corresponding to a blowoff velocity of 16.5 m/s.</p>
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<p>Global OH*-CL signal intensity and the occurrence probability of blowoff precursors under various FMFRT amplitudes at a mean fuel mass flow rate of 0.142 g/s.</p>
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26 pages, 33259 KiB  
Article
Automatic High-Resolution Operational Modal Identification of Thin-Walled Structures Supported by High-Frequency Optical Dynamic Measurements
by Tongfa Deng, Yuexin Wang, Jinwen Huang, Maosen Cao and Dragoslav Sumarac
Materials 2024, 17(20), 4999; https://doi.org/10.3390/ma17204999 - 12 Oct 2024
Viewed by 948
Abstract
High-frequency optical dynamic measurement can realize multiple measurement points covering the whole surface of the thin-walled structure, which is very useful for obtaining high-resolution spatial information for damage localization. However, the noise and low calculation efficiency seriously hinder its application to real-time, online [...] Read more.
High-frequency optical dynamic measurement can realize multiple measurement points covering the whole surface of the thin-walled structure, which is very useful for obtaining high-resolution spatial information for damage localization. However, the noise and low calculation efficiency seriously hinder its application to real-time, online structural health monitoring. To this end, this paper proposes a novel high-resolution frequency domain decomposition (HRFDD) modal identification method, combining an optical system with an accelerometer for measuring high-accuracy vibration response and introducing a clustering algorithm for automated identification to improve efficiency. The experiments on the cantilever aluminum plate were carried out to evaluate the effectiveness of the proposed approach. Natural frequency and damping ratios were obtained by the least-squares complex frequency domain (LSCF) method to process the acceleration responses; the high-resolution mode shapes were acquired by the singular value decomposition (SVD) processing of global displacement data collected by high-speed cameras. Finally, the complete set of the first nine order modal parameters for the plate within the frequency range of 0 to 500 Hz has been determined, which is closely consistent with the results obtained from both experimental modal analysis and finite element analysis; the modal parameters could be automatically picked up by the DBSCAN algorithm. It provides an effective method for applying optical dynamic technology to real-time, online structural health monitoring, especially for obtaining high-resolution mode shapes. Full article
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Graphical abstract

Graphical abstract
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<p>High-frequency optical dynamic measurement system for high-resolution modal identification.</p>
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<p>Flowchart of the improved operating modal analysis approach.</p>
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<p>The results of clustering: (<b>a</b>) K-means and (<b>b</b>) DBSCAN.</p>
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<p>Equivalent simplified mode of ten-story shear frame.</p>
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<p>Stability diagram of frame (based on displacement response <math display="inline"><semantics> <mrow> <msub> <mi>x</mi> <mn>8</mn> </msub> </mrow> </semantics></math> with 5% noise).</p>
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<p>The automated clustering results of frame true poles.</p>
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<p>Calculated value and theoretical value of mode shapes.</p>
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<p>The HRFDD vibration testing system (① aluminum plate, ② customized fixture, ③ impact hammer, ④ lighting, ⑤ high-speed cameras, ⑥ acceleration sensor 1A111E, ⑦ laptop, ⑧ signal analyzer DH5928).</p>
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<p>Layout of displacement measuring points on the aluminum plate.</p>
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<p>The magnitude of the excitation force.</p>
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<p>Acceleration response of the aluminum plate.</p>
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<p>The time–displacement response in the Z direction at four testing points on the surface of the plate.</p>
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<p>Stability diagram (based on input excitation and output acceleration response).</p>
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<p>PSD function curve of PP: (<b>a</b>) unprocessed noisy PSD function curve; (<b>b</b>) windowed PSD curve.</p>
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<p>Amplitude curves of several PSD functions.</p>
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<p>The first four singular value spectrum curves.</p>
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<p>Stability diagram (based on displacement data measured by high-speed camera).</p>
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<p>Stability diagram of the plate (based on a set of acceleration response data).</p>
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<p>True pole automated clustering results of the rectangular plate.</p>
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<p>Comparison of MAC values obtained by comparing mode shapes obtained from FEA with those obtained from operational modal analysis (PP, EFDD, LSCF, and the proposed HRFDD).</p>
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