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30 pages, 11200 KiB  
Article
Shock Waves in Ion-Beam-Depleted Spin-Polarized Quantum Plasma with Ionic Pressure Anisotropy
by Manoj K. Deka, Balaram Pradhan, Apul N. Dev, Deepsikha Mahanta, Jalil Manafian and Khaled H. Mahmoud
Plasma 2025, 8(1), 3; https://doi.org/10.3390/plasma8010003 - 8 Jan 2025
Viewed by 302
Abstract
In this study, the effects of pressure anisotropy and viscosity on the propagation of shock waves in spin-polarized degenerate quantum magnetoplasma are studied under the influence of the streaming energy of ion beams. The effects of different suitable plasma parameters on the shock [...] Read more.
In this study, the effects of pressure anisotropy and viscosity on the propagation of shock waves in spin-polarized degenerate quantum magnetoplasma are studied under the influence of the streaming energy of ion beams. The effects of different suitable plasma parameters on the shock wave’s potential profile are studied using the steady state solution of the Zakharov–Kuznetsov–Burgers (Z–K–B) equation, as well as the numerical simulation of the governing non-linear Z–K–B equation. First-order analysis of the non-linear wave propagation depicted a new beam-induced stable mode whose Mach number may be subsonic or supersonic depending on the anisotropic pressure combination in the presence of different spin density polarization ratios. This is the first observation of this new beam-induced stable mode in ion beam plasma, apart from the other existing modes of ion beam plasma systems, namely, the fast beam mode, the slow beam mode, the inherent ion acoustic mode, and the coupled mode, which also has unique propagation characteristics compared to the other modes. The spin density polarization ratio of spin-up and spin-down electrons have an unprecedented effect on the polarity and the direction of propagation of different shock wave modes in such plasma systems. Apart from the spin effect, anisotropic pressure combinations, as well as the viscosity of ions and ion beams, also play an outstanding role in controlling the nature of propagation of shock waves, especially in the newly detected beam-induced stable mode, and depending on the viscosity parameters of ions and ion beams, both oscillatory and monotonic shock waves can propagate in such plasma. Full article
Show Figures

Figure 1

Figure 1
<p>(<b>a</b>) Mach number variation of different ion beam modes with normalized beam velocity when the concentration of spin-up electrons is more than the spin-down electrons with parallel pressure of beam ions higher than the ions. The features of all the modes are sketched. The inset of (<b>a</b>) shows the variation of the stable beam mode with beam velocity. (<b>b</b>) Mach number variation of different ion beam modes with normalized beam velocity when the concentration of spin-up electrons is equal to the spin-down electrons with parallel pressure of beam ions higher than the ions. The inset of (<b>b</b>) shows the variation of the stable beam mode with beam velocity. Here, it is to be noted that <math display="inline"><semantics> <mrow> <msub> <mi>V</mi> <mrow> <mi>b</mi> <mn>0</mn> </mrow> </msub> <mo>=</mo> <mrow> <mrow> <msub> <mi>V</mi> <mi>b</mi> </msub> </mrow> <mo>/</mo> <mrow> <msub> <mi>C</mi> <mi>s</mi> </msub> </mrow> </mrow> </mrow> </semantics></math>.</p>
Full article ">Figure 2
<p>(<b>a</b>) Mach number variation of different ion beam modes with normalized beam velocity when the concentration of spin-up electrons is more than the spin-down electrons with parallel pressure of ions lower than the beam ions. The features of all the modes are sketched. The inset of (<b>a</b>) shows the variation of the stable beam mode with beam velocity. (<b>b</b>) Mach number variation of different ion beam modes with normalized beam velocity when the concentration of spin-up electrons is equal to the spin-down electrons with parallel anisotropy of ions lower than the beam ions. The inset of (<b>b</b>) shows the variation of the stable beam mode with beam velocity. Here, it is to be noted that <math display="inline"><semantics> <mrow> <msub> <mi>V</mi> <mrow> <mi>b</mi> <mn>0</mn> </mrow> </msub> <mo>=</mo> <mrow> <mrow> <msub> <mi>V</mi> <mi>b</mi> </msub> </mrow> <mo>/</mo> <mrow> <msub> <mi>C</mi> <mi>s</mi> </msub> </mrow> </mrow> </mrow> </semantics></math>.</p>
Full article ">Figure 3
<p>(<b>a</b>) Variation in normalized phase velocity (Mach Number) of different ion beam modes with normalized beam velocity when the concentration of spin-up electrons is more than the spin-down electrons with parallel pressure of ions is equal to the beam ions. The features of all the modes are sketched. The inset of (<b>a</b>) shows the variation in the stable beam mode with beam velocity. (<b>b</b>) Variation in normalized phase velocity (Mach Number) of different ion beam modes with normalized beam velocity when the concentration of spin-up electrons is equal to the spin-down electrons with parallel anisotropy of ions is equal to the beam ions. The inset of (<b>b</b>) shows the variation of the stable beam mode with beam velocity. Here, it is to be noted that <math display="inline"><semantics> <mrow> <msub> <mi>V</mi> <mrow> <mi>b</mi> <mn>0</mn> </mrow> </msub> <mo>=</mo> <mrow> <mrow> <msub> <mi>V</mi> <mi>b</mi> </msub> </mrow> <mo>/</mo> <mrow> <msub> <mi>C</mi> <mi>s</mi> </msub> </mrow> </mrow> </mrow> </semantics></math>.</p>
Full article ">Figure 4
<p>(<b>a</b>) Numerical evolution of shock wave potential profile of fast beam mode with parallel pressure of beam ions higher than the ions for different values of <math display="inline"><semantics> <mrow> <mi>τ</mi> </mrow> </semantics></math>. (<b>b</b>) Numerical evolution of shock wave potential profile of slow beam mode with parallel pressure of beam ions higher than the ions for different <math display="inline"><semantics> <mrow> <mi>τ</mi> </mrow> </semantics></math>. Here, we have considered <math display="inline"><semantics> <mrow> <mrow> <mrow> <msub> <mi>V</mi> <mi>b</mi> </msub> </mrow> <mo>/</mo> <mrow> <msub> <mi>C</mi> <mi>s</mi> </msub> </mrow> </mrow> <mo>=</mo> <mn>2.5</mn> </mrow> </semantics></math>.</p>
Full article ">Figure 5
<p>(<b>a</b>) Numerical evolution of shock wave potential profile of ion acoustic mode with parallel pressure of beam ions higher than the ions for different values of <math display="inline"><semantics> <mrow> <mi>τ</mi> </mrow> </semantics></math>. (<b>b</b>) Variation in shock wave potential profile of ion acoustic mode with parallel pressure of beam ions higher than the ions for different <math display="inline"><semantics> <mrow> <mi>τ</mi> </mrow> </semantics></math>.</p>
Full article ">Figure 6
<p>(<b>a</b>) Numerical evolution of shock wave potential profile of stable beam mode with parallel pressure of beam ions higher than the ions for different values of <math display="inline"><semantics> <mrow> <mi>τ</mi> </mrow> </semantics></math>. (<b>b</b>) Variation in shock wave potential profile of stable beam mode with parallel pressure of beam ions higher than the ions for different <math display="inline"><semantics> <mrow> <mi>τ</mi> </mrow> </semantics></math>.</p>
Full article ">Figure 7
<p>(<b>a</b>) Variation in shock wave potential profile of fast beam mode with parallel pressure of beam ions higher than the ions for a different combination of perpendicular pressure anisotropy and viscosity parameter of ion and ion beams when the concentration of spin-up electrons is equal to the spin-down electrons, (<b>b</b>) Variation in shock wave potential profile of fast beam mode with parallel pressure of beam ions is higher than the ions for a different combination of perpendicular pressure anisotropy and viscosity parameter of ion and ion beams when the concentration of spin-up electron is more than the spin-down electrons. Here, we have considered <math display="inline"><semantics> <mrow> <mrow> <mrow> <msub> <mi>V</mi> <mi>b</mi> </msub> </mrow> <mo>/</mo> <mrow> <msub> <mi>C</mi> <mi>s</mi> </msub> </mrow> </mrow> <mo>=</mo> <mn>2</mn> </mrow> </semantics></math>.</p>
Full article ">Figure 8
<p>(<b>a</b>) Variation in shock wave potential profile of stable beam mode with parallel pressure of beam ions higher than the ions for <b>a</b> different combination of perpendicular pressure anisotropy and viscosity parameter of ion and ion beams when the concentration of spin-up electron is equal to the spin-down electrons. (<b>b</b>) Variation in shock wave potential profile of stable beam mode with parallel pressure of beam ions is higher than the ions for a different combination of perpendicular pressure anisotropy and viscosity parameter of ion and ion beams when the concentration of spin-up electron is more than the spin-down electrons.</p>
Full article ">Figure 9
<p>(<b>a</b>) Variation in shock wave potential profile of stable beam mode with parallel pressure of beam ions higher than the ions for <b>a</b> different combination of perpendicular pressure anisotropy and viscosity parameter of ion and ion beams when the concentration of spin-up electron is equal to the spin-down electrons. (<b>b</b>) Variation in shock wave potential profile of stable beam mode with parallel pressure of beam ions higher than the ions for a different combination of perpendicular pressure anisotropy and viscosity parameter of ion and ion beams when the concentration of spin-up electron is more than the spin-down electrons.</p>
Full article ">Figure 10
<p>(<b>a</b>) Variation in shock wave potential profile ion acoustic mode with parallel pressure of beam ions higher than the ions for <b>a</b> different combination of perpendicular pressure anisotropy and viscosity parameter of ion and ion beams when the concentration of spin-up electrons is equal to the spin-down electrons, (<b>b</b>) Variation in shock wave potential profile of Ion Acoustic mode with parallel pressure of beam ions is higher than the ions for a different combination of perpendicular pressure anisotropy and viscosity parameter of ion and ion beams when the concentration of spin-up electrons is more than the spin-down electrons.</p>
Full article ">Figure 11
<p>(<b>a</b>) Variation in shock wave potential profile ion acoustic mode with parallel pressure of beam ions is higher than the ions for <b>a</b> different combination of perpendicular pressure anisotropy and viscosity parameter of ion and ion beams when the concentration of spin-up electrons is equal to the spin-down electrons for higher beam velocity, (<b>b</b>) Variation in shock wave potential profile of ion acoustic mode with parallel pressure of beam ions higher than the ions for <b>a</b> different combination of perpendicular pressure anisotropy and viscosity parameter of ion and ion beams when the concentration of spin-up electrons is more than the spin-down electrons for higher beam velocity.</p>
Full article ">Figure 12
<p>(<b>a</b>) Variation in shock wave potential profile of slow beam mode with parallel pressure of beam ions higher than the ions for a different combination of perpendicular pressure anisotropy and viscosity parameter of ion and ion beams when the concentration of spin-up electrons is equal to the spin-down electrons. (<b>b</b>) Variation in shock wave potential profile of slow beam mode with parallel pressure of beam ions is higher than the ions for <b>a</b> different combination of perpendicular pressure anisotropy and viscosity parameter of ion and ion beams when the concentration of spin-up electrons is more than the spin-down electrons. Here, we have considered <math display="inline"><semantics> <mrow> <mrow> <mrow> <msub> <mi>V</mi> <mi>b</mi> </msub> </mrow> <mo>/</mo> <mrow> <msub> <mi>C</mi> <mi>s</mi> </msub> </mrow> </mrow> <mo>=</mo> <mn>2.5</mn> </mrow> </semantics></math>.</p>
Full article ">Figure 13
<p>(<b>a</b>) Variation in shock wave potential profile of fast beam mode with parallel pressure of beam ions greater than the ions for different combination of perpendicular pressure anisotropy and viscosity parameter of ion and ion beams when the concentration of spin-up electrons is equal to the spin-down electrons for the case <math display="inline"><semantics> <mrow> <msub> <mi>μ</mi> <mi>b</mi> </msub> <mo>=</mo> <mn>0.8</mn> </mrow> </semantics></math>. (<b>b</b>) Variation in shock wave potential profile of slow beam mode with parallel pressure of beam ions greater than the ions for different combination of perpendicular pressure and viscosity parameter of ion and ion beams when the concentration of spin-up electrons is equal to the spin-down electrons for the case <math display="inline"><semantics> <mrow> <msub> <mi>μ</mi> <mi>b</mi> </msub> <mo>=</mo> <mn>0.8</mn> </mrow> </semantics></math>. (<b>c</b>) Variation in shock wave potential profile of stable beam mode with parallel pressure of beam ions greater than the ions for different combination of perpendicular pressure and viscosity parameter of ion and ion beams when the concentration of spin-up electrons is equal to the spin-down electrons for the case <math display="inline"><semantics> <mrow> <msub> <mi>μ</mi> <mi>b</mi> </msub> <mo>=</mo> <mn>0.8</mn> </mrow> </semantics></math>. (<b>d</b>) Variation in shock wave potential profile of Ion Acoustic mode with parallel pressure of beam ions greater than the ions for different combination of perpendicular pressure and viscosity parameter of ion and ion beams when the concentration of spin-up electron is equal to the spin-down electrons for the case <math display="inline"><semantics> <mrow> <msub> <mi>μ</mi> <mi>b</mi> </msub> <mo>=</mo> <mn>0.8</mn> </mrow> </semantics></math>. Here, we have considered <math display="inline"><semantics> <mrow> <mrow> <mrow> <msub> <mi>V</mi> <mi>b</mi> </msub> </mrow> <mo>/</mo> <mrow> <msub> <mi>C</mi> <mi>s</mi> </msub> </mrow> </mrow> <mo>=</mo> <mn>2.5</mn> </mrow> </semantics></math>.</p>
Full article ">Figure 14
<p>(<b>a</b>) Numerical evolution of shock wave potential profile of fast beam mode with parallel pressure of beam ions higher than the ions for different combinations of perpendicular pressure ion and ion beams with viscosity of beam ions higher than the positive ions, (<b>b</b>) Variation in shock wave potential profile of fast beam mode with parallel pressure of beam ions higher than the ions for different combination of perpendicular pressures of ion and ion beams with viscosity of positive ions higher than the beam ions. Here, we have considered <math display="inline"><semantics> <mrow> <mrow> <mrow> <msub> <mi>V</mi> <mi>b</mi> </msub> </mrow> <mo>/</mo> <mrow> <msub> <mi>C</mi> <mi>s</mi> </msub> </mrow> </mrow> <mo>=</mo> <mn>2.5</mn> </mrow> </semantics></math>.</p>
Full article ">Figure 15
<p>(<b>a</b>) Numerical evolution of shock wave potential profile of slow beam mode with parallel pressure of beam ions higher than the ions for different combinations of perpendicular pressure ion and ion beams with the viscosity of beam ions higher than the positive ions, (<b>b</b>) Variation in shock wave potential profile of slow beam mode with parallel pressure of beam ions higher than the ions for different combination of perpendicular pressures of ion and ion beams with viscosity of positive ions higher than the beam ions. Here, we have considered <math display="inline"><semantics> <mrow> <mrow> <mrow> <msub> <mi>V</mi> <mi>b</mi> </msub> </mrow> <mo>/</mo> <mrow> <msub> <mi>C</mi> <mi>s</mi> </msub> </mrow> </mrow> <mo>=</mo> <mn>2.5</mn> </mrow> </semantics></math>.</p>
Full article ">Figure 16
<p>(<b>a</b>) Numerical evolution of shock wave potential profile of slow beam mode with parallel pressure of beam ions higher than the ions for different combinations of perpendicular pressure and viscosity parameter of ion and ion beams with viscosity of beam ions higher than the positive ions. (<b>b</b>) Variation in shock wave potential profile of slow beam mode with parallel pressure of beam ions higher than the ions for different combination of perpendicular pressure of ion and ion beams with viscosity of positive ions higher than the beam ions. Here, we have considered <math display="inline"><semantics> <mrow> <mrow> <mrow> <msub> <mi>V</mi> <mi>b</mi> </msub> </mrow> <mo>/</mo> <mrow> <msub> <mi>C</mi> <mi>s</mi> </msub> </mrow> </mrow> <mo>=</mo> <mn>2.5</mn> </mrow> </semantics></math>.</p>
Full article ">Figure 17
<p>(<b>a</b>) Numerical evolution of shock wave potential profile of ion acoustic mode with parallel pressure of beam ions higher than the ions for a different combination of perpendicular pressure and viscosity parameter of ion and ion beams with the viscosity of beam ions higher than the positive ions. (<b>b</b>) Variation in shock wave potential profile of ion acoustic mode with parallel pressure of beam ions higher than the ions for a different combination of perpendicular pressure of ion and ion beams with the viscosity of positive ions higher than the beam ions. Here, we have considered <math display="inline"><semantics> <mrow> <mrow> <mrow> <msub> <mi>V</mi> <mi>b</mi> </msub> </mrow> <mo>/</mo> <mrow> <msub> <mi>C</mi> <mi>s</mi> </msub> </mrow> </mrow> <mo>=</mo> <mn>0.4</mn> </mrow> </semantics></math>.</p>
Full article ">Figure 18
<p>(<b>a</b>) Numerical evolution of shock wave potential profile of stable beam mode with parallel pressure of beam ions higher than the ions for different combinations of perpendicular pressure of ion and ion beams with viscosity of positive ions higher than the beam ions. (<b>b</b>) Numerical evolution of shock wave potential profile of stable beam mode with higher parallel pressure of beam ions and the positive ions for different combination of perpendicular pressure of ion and ion beams with viscosity of positive ions higher than the beam ions. Here, we have considered <math display="inline"><semantics> <mrow> <mrow> <mrow> <msub> <mi>V</mi> <mi>b</mi> </msub> </mrow> <mo>/</mo> <mrow> <msub> <mi>C</mi> <mi>s</mi> </msub> </mrow> </mrow> <mo>=</mo> <mn>2.5</mn> </mrow> </semantics></math>.</p>
Full article ">Figure 19
<p>(<b>a</b>) Numerical evolution of shock wave potential profile of stable beam mode with parallel pressure of beam ions higher than the ions for different combinations of perpendicular pressure of ion and ion beams with viscosity of beam ions higher than the positive ions. (<b>b</b>) Numerical evolution of shock wave potential profile of stable beam mode with equal and higher parallel pressure of both the positive ions and beam ions for different combination of perpendicular pressure of ion and ion beams with viscosity of beam ions higher than the positive ions. Here, we have considered <math display="inline"><semantics> <mrow> <mrow> <mrow> <msub> <mi>V</mi> <mi>b</mi> </msub> </mrow> <mo>/</mo> <mrow> <msub> <mi>C</mi> <mi>s</mi> </msub> </mrow> </mrow> <mo>=</mo> <mn>2.5</mn> </mrow> </semantics></math>.</p>
Full article ">
21 pages, 4025 KiB  
Article
What Is Grazing Time? Insights from the Acoustic Signature of Goat Jaw Activity in Wooded Landscapes
by Eugene David Ungar and Reuven Horn
Sensors 2025, 25(1), 8; https://doi.org/10.3390/s25010008 - 24 Dec 2024
Viewed by 260
Abstract
Acoustic monitoring facilitates the detailed study of herbivore grazing by generating a timeline of sound bursts associated with jaw movements (JMs) that perform bite or chew actions. The unclassified stream of JM events was used here in an observational study to explore the [...] Read more.
Acoustic monitoring facilitates the detailed study of herbivore grazing by generating a timeline of sound bursts associated with jaw movements (JMs) that perform bite or chew actions. The unclassified stream of JM events was used here in an observational study to explore the notion of “grazing time”. Working with shepherded goat herds in a wooded landscape, a horn-based acoustic sensor with a vibration-type microphone was deployed on a volunteer animal along each of 12 foraging routes. The software-generated timeline of unclassified JMs contained a total of 334,582 events. After excluding rumination bouts, minutely JM rates showed a broad, non-normal distribution, with an overall mean of 61 JM min−1. The frequency distribution of inter-JM interval values scaled logarithmically, with a peak in the region of 0.43 s representing a baseline interval that generates the unconstrained, more-or-less regular, rhythm of jaw movement (≈140 JM min−1). This rhythm was punctuated by interruptions, for which duration scaled logarithmically, and which were primarily related to the search phase of the intake process. The empirical time accumulation curve shows the contribution of the inter-JM interval to the total foraging time and provides a penetrating profile of how the animal interacted with the foraging environment. The sum total of time along a foraging route spent at a near-potential JM rate was only ≈1 h, whereas sub-potential rates containing intervals as long as ≈30 s accounted for the bulk of the foraging route. The dimensionless behavioral grazing intensity was defined as the product of the number of ingestive JMs performed and the baseline interval, divided by the duration of the foraging route (excluding rumination). Values were mostly <0.5 for the foraging routes examined. This has implications for how animal presence should be translated to grazing pressure and for how long animals need to forage to meet their nutritional requirements. Full article
Show Figures

Figure 1

Figure 1
<p>Photograph of goat with acoustic sensor attached to left horn. Taken on 6 April 2014, in the holding pen of herd KDE prior to commencement of the foraging route.</p>
Full article ">Figure 2
<p>Examples of the waveform obtained via the acoustic monitoring of grazing goats in a Mediterranean shrubby and woody rangeland. The waveforms are a graphical representation of the pattern of sound pressure variation (amplitude) in the time domain. Each panel shows a 30 s segment of relatively active jaw activity, identified by herd (3-letter code defined in <a href="#sensors-25-00008-t001" class="html-table">Table 1</a>), season (wet or dry), and date. Times are hh:mm:ss.</p>
Full article ">Figure 3
<p>Rumination patterns of jaw movement from time-based and event-based perspectives. Panels (<b>A</b>–<b>C</b>) are waveforms of the sound signal taken from one foraging route (KDE, Dry, 29 October 2013) at different scales of enlargement spanning 30, 4, and 2 min, respectively. Panel (<b>D</b>) shows the waveform of a 7 min bout of rumination from a different foraging route (KDE, Wet, 6 April 2014); panels (<b>E</b>,<b>F</b>) show the corresponding event-based plot; corresponding boli have matching lower-case letters.</p>
Full article ">Figure 4
<p>Frequency distribution of the inter-jaw-movement interval (s) for (<b>A</b>) rumination and (<b>B</b>) grazing, with logarithmic scaling. The extreme low end of the distribution may be due in part to false positive identifications of jaw movements. In the outlier box plots, the box center line is the median; box ends are 1st and 3rd quartiles; whiskers extend from box ends to the outermost value within the 1st/3rd quartile –/+ 1.5 × interquartile range; the center line of the confidence diamond is the mean and the lower and upper 95% of the mean (the left and right points of the diamond); and the bracket above box is the shortest half—the densest 50% of observations.</p>
Full article ">Figure 5
<p>Event-based plots of grazing (non-ruminatory) jaw activity showing different patterns and degrees of intensity. The herd ID, season, date, and time interval between the two arrows are indicated. Panel (<b>A</b>) shows a run of at least 100 consecutive jaw movements with an inter-jaw-movement interval &lt;1 s (horizontal line); in panels (<b>B</b>,<b>C</b>), the threshold was increased to 2 s and 5 s, respectively; panel (<b>D</b>) shows short segments bounded by intervals &gt;5 s; panel (<b>E</b>) shows a highly erratic pattern of intervals.</p>
Full article ">Figure 6
<p>The relationship between run duration (i.e., sum of intervals) (s) and run length (i.e., number of intervals) (-) for three thresholds of the inter-jaw-movement interval: (<b>A</b>) 1 s; (<b>B</b>) 2 s; (<b>C</b>) 5 s. Note that the panels are independently scaled.</p>
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<p>The frequency distribution of non-zero, minute RJM for the following: (<b>A</b>) the pooled dataset containing both rumination (including uncertain rumination) and grazing (<span class="html-italic">n</span> = 5096, median = 66 JM min<sup>−1</sup>); (<b>B</b>) the dataset containing rumination (including uncertain rumination) only (<span class="html-italic">n</span> = 359, median = 81 JM min<sup>−1</sup>); (<b>C</b>) the dataset containing grazing only (<span class="html-italic">n</span> = 4737, median = 64 JM min<sup>−1</sup>).</p>
Full article ">Figure 8
<p>The CDF of inter-jaw-movement intervals designated as grazing (i.e., not rumination), for individual foraging routes. The interval is on the logarithmic scale. The insert shows an enlargement containing the interval range of 0.1–5 s.</p>
Full article ">Figure 9
<p>Empirical time accumulation curves showing the cumulative ascending ranked interval of jaw activity designated as grazing (i.e., non-rumination), for the 12 foraging routes. The interval is on the logarithmic scale.</p>
Full article ">
18 pages, 4868 KiB  
Article
A Simulation Study of Low-Intensity Focused Ultrasound for Modulating Rotational Sense Through Acoustic Streaming in Semicircular Canal: A Pilot Study
by Sion Cha and Wooksung Kim
Appl. Sci. 2024, 14(23), 11432; https://doi.org/10.3390/app142311432 - 9 Dec 2024
Viewed by 545
Abstract
This study explores the feasibility of using low-intensity focused ultrasound (LIFU) to induce rotational sensations in the human semicircular canal (SCC) through the acoustic streaming effect. Existing vestibular stimulation methods, such as galvanic vestibular stimulation (GVS), caloric vestibular stimulation (CVS), and magnetic vestibular [...] Read more.
This study explores the feasibility of using low-intensity focused ultrasound (LIFU) to induce rotational sensations in the human semicircular canal (SCC) through the acoustic streaming effect. Existing vestibular stimulation methods, such as galvanic vestibular stimulation (GVS), caloric vestibular stimulation (CVS), and magnetic vestibular stimulation (MVS), face limitations in spatial and temporal resolution, with unclear mechanisms. This study investigates whether LIFU can overcome these limitations by modulating endolymph motion within SCC. A 3D finite element model was constructed to simulate the effects of LIFU-induced acoustic streaming on SCC (particularly the endolymph), with thermal effects evaluated to ensure safety. Fluid–structure interaction (FSI) was used to analyze the relationship between endolymph flow and cupula deformation. By adjusting the focal point of the ultrasound transducer, we were able to alter fluid flow pattern, which resulted in variations in cupula displacement. The results demonstrated that LIFU successfully induces fluid motion in SCC without exceeding thermal safety limits (<1 °C), suggesting its potential for controlling rotational sensations, with cupula displacement exceeding 1 μm. This novel approach enhances the understanding of LIFU’s thermal and neuromodulatory effects on the vestibular system, and thereby offers promising implications for future therapeutic applications. Full article
Show Figures

Figure 1

Figure 1
<p>(<b>a</b>) 3D structure of the SCC model, including the cupula and endolymph. The red cross-section represents the interface between the cupula and endolymph, which will deform in subsequent analyses. The ultrasound radiation is emitted in the positive z-direction. (<b>b</b>) FEM domain of the numerical model in the xz-plane, highlighting a horizontal SCC filled with endolymph fluid and the cupula. The structure is centered at the coordinates (0, 0, 40).</p>
Full article ">Figure 2
<p>Comparison of the present model with experimental and numerical results: (<b>a</b>) Streaming velocity in water caused by focused ultrasound compared with Mitome [<a href="#B53-applsci-14-11432" class="html-bibr">53</a>], and (<b>b</b>) temperature rise in human tissue exposed to focused ultrasound compared with Huang et al. [<a href="#B31-applsci-14-11432" class="html-bibr">31</a>]. In both graphs, the black solid line represents the results from our model, while the red circles indicate the results from other studies.</p>
Full article ">Figure 3
<p>Comparison between the 2D axisymmetric model and the FEM-BEM combined model. The result compares the total acoustic pressure along the axial distance and shows similar trends with minimal error.</p>
Full article ">Figure 4
<p>(<b>a</b>) Axial direction results showing the focal distance and normalized intensity for transducers at 400 kHz, 600 kHz, and 800 kHz. Normalization was applied using the maximum intensity of 38.21 W/cm<sup>2</sup> at 800 kHz. (<b>b</b>) Lateral direction results calculated along the line defined by y = 0, corresponding to the z-axis where the intensity was maximum.</p>
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<p>Acoustic intensity profile showing the maximum intensity near the ampulla in the SCC at (<b>a</b>) 400 kHz, (<b>b</b>) 600 kHz, and (<b>c</b>) 800 kHz.</p>
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<p>Acoustic energy dissipation density at (<b>a</b>) 400 kHz, (<b>b</b>) 600 kHz, and (<b>c</b>) 800 kHz. The area of concentrated dissipation decreases as the frequency increases, similar to the intensity.</p>
Full article ">Figure 7
<p>Visualization of acoustic streaming patterns in the endolymph of the SCC induced by focused ultrasound at three different frequencies: (<b>a</b>) 400 kHz, (<b>b</b>) 600 kHz, and (<b>c</b>) 800 kHz. The results are shown on the xz-plane (y = 0), which represents a cross-sectional slice of the SCC structure perpendicular to the y-axis. The scale factors for each frequency are set at 500,000, 50,000, and 10,000, respectively.</p>
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<p>Three-dimensional visualization of cupula displacement caused by acoustic streaming in the endolymph at three different frequencies: (<b>a</b>) 400 kHz, (<b>b</b>) 600 kHz, and (<b>c</b>) 800 kHz. The displacement results are shown on the surface of the cupula, with the center of the cupula positioned at (0, 0).</p>
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<p>(<b>a</b>) Temperature distribution along the axial distance (z-axis) at 1 second for three different frequencies: 400 kHz, 600 kHz, and 800 kHz. The maximum temperature increases are shown at 35.2 mm, 37.1 mm, and 39.4 mm for each frequency, respectively. (<b>b</b>) Time-dependent temperature rises during and after 1 second of ultrasound exposure, with a total time of 5 seconds. Each point is at the location where the maximum temperature was recorded.</p>
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<p>Comparison of temperature changes at 800 kHz with and without the presence of the SCC. The graph shows the temperature variation in the temporal bone at the same point (z = 39.4 mm) in both cases and in the endolymph region (z = 42 mm) when the SCC is present.</p>
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<p>Cupula displacement occurs when the focal position of the ultrasound transducer is shifted along the x-axis from x = −3 mm to x = 3 mm. (<b>a</b>–<b>c</b>) When the focus is positioned on the left side of the SCC center (x &lt; 0), the dissipated energy generates endolymph flow in the clockwise direction. (<b>d</b>–<b>f</b>) Conversely, when the focus is positioned on the right side (x &gt; 0), it generates endolymph flow in the counterclockwise direction.</p>
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18 pages, 11716 KiB  
Article
Performance Analysis of Underwater Radiofrequency Communication in Seawater: An Experimental Study
by Raji Alahmad, Hussam Alraie, Ryosuke Hasaba, Kazuhiro Eguchi, Tohlu Matsushima, Yuki Fukumoto and Kazuo Ishii
J. Mar. Sci. Eng. 2024, 12(11), 2104; https://doi.org/10.3390/jmse12112104 - 20 Nov 2024
Viewed by 692
Abstract
Communication with the underwater vehicles during their tasks is one of the most important issues. The need for real-time data transfer raises the necessity of developing communication systems. Conventional underwater communication systems, such as acoustic systems, cannot satisfy applications that need a high [...] Read more.
Communication with the underwater vehicles during their tasks is one of the most important issues. The need for real-time data transfer raises the necessity of developing communication systems. Conventional underwater communication systems, such as acoustic systems, cannot satisfy applications that need a high transmission data rate. In this study, we investigate the radio frequency communication system in seawater, which is crucial for real-time data transfer with underwater vehicles. The experiments were in a water tank full of seawater and a real environment in the ocean. Three types of antennae were used: loop antenna, wire antenna, and helical antenna. An Autonomous Underwater Vehicle (AUV) is used as a transmitter to measure the transmission rate as a function of distance. The helical antenna showed better performance regarding the coverage area. Furthermore, the AUV could move freely within the helical and capture live video streaming successfully. This investigation underscores the potential of radio frequency communication systems for enhancing underwater vehicle operations, offering promising avenues for future research and practical implementation. Full article
(This article belongs to the Special Issue Intelligent Approaches to Marine Engineering Research)
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<p>The layout connection between the AUV and the base antenna.</p>
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<p>The structure of the antennas used in this research.</p>
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<p>Experiment design of the loop antenna. The origin point is the center of the base antenna, and the <span class="html-italic">z</span>-axis is the anti-gravity direction.</p>
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<p>Experiment design of the U-UWA antenna. The origin position is the horizontal center of the pool with a depth of 0.5 m from the bottom.</p>
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<p>Experiment design of the helical antenna. The antenna surrounded the pool with two loops. The origin position is the horizontal center of the pool with a depth of 0.5 m.</p>
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<p>Experiment design of the sea experiment. Loop antennas were used for both the station and AUV; the base antenna was fixed on a specific depth by floating, and both antennas were connected to the boat by an optical cable.</p>
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<p>The three designed antenna models.</p>
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<p>Comparison of S11-parameters of the designed antennas.</p>
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<p>The magnetic field of the three antennas, top view.</p>
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<p>The magnetic field of the three antennas, front view.</p>
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<p>The magnetic field of the three antennas, left view.</p>
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<p>Transmission rate between the transmitter and receiver using loop antenna. The results of using TCP protocol.</p>
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<p>Transmission rate between the transmitter and receiver using loop antenna. The results of using the UDP protocol.</p>
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<p>Transmission rate between the transmitter and receiver using U-UWA. The results of using TCP protocol.</p>
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<p>Transmission rate between the transmitter and receiver using U-UWA. The results of using the UDP protocol.</p>
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<p>Transmission rate between the transmitter and receiver using a helical antenna. The results of using TCP protocol.</p>
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<p>Transmission rate between the transmitter and receiver using a helical antenna. The results of using the UDP protocol.</p>
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<p>Real-time transmission rate while the AUV hovers randomly in the pool using U-UWA.</p>
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<p>Real-time transmission rate while the AUV hovers randomly in the pool using a helical antenna.</p>
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<p>The depth of the base antenna and AUV antenna during the video streaming in the ocean. The case when the base antenna is under the AUV.</p>
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<p>Snapshots for the live video streaming in the ocean, the video captured by optical wired for reference, and RF link using UDP protocol. The framerate is 25 fps, the total video length is 50 seconds, and the snapshot sampling is 2 s.</p>
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<p>Framerate of the captured video in both wire and wireless communication.</p>
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<p>The depth of the base antenna and AUV antenna during the video streaming in the ocean. The case when AUV is under the base antenna.</p>
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20 pages, 6853 KiB  
Article
Upper Ocean Thermodynamic Response to Coupling Currents to Wind Stress over the Gulf Stream
by Jackie May and Mark A. Bourassa
J. Mar. Sci. Eng. 2024, 12(11), 1994; https://doi.org/10.3390/jmse12111994 - 5 Nov 2024
Viewed by 953
Abstract
We use high-resolution coupled atmosphere–ocean model simulations over the Gulf Stream extension region during a winter season to examine the upper ocean thermodynamic response to including current feedback to atmospheric wind stress. We demonstrate that a model that includes current feedback leads to [...] Read more.
We use high-resolution coupled atmosphere–ocean model simulations over the Gulf Stream extension region during a winter season to examine the upper ocean thermodynamic response to including current feedback to atmospheric wind stress. We demonstrate that a model that includes current feedback leads to significant changes in the structure and transport of heat throughout the upper ocean in comparison to the same model without current feedback. We find that including the current feedback leads to changes in the upper ocean temperature pattern that match the vorticity pattern. Areas with cyclonic ocean vorticity, typically north of the Gulf Stream extension, correspond to areas with warmer temperatures throughout the water column. Areas with anticyclonic ocean vorticity, typically south of the Gulf Stream extension, correspond to areas with cooler temperatures throughout the water column. We also find that including current feedback leads to an overall reduction in the submesoscale vertical heat flux spectra across all spatial scales, with differences in the submesoscale vertical heat flux corresponding to SST minus mixed layer temperature differences. The direct impact of current feedback on the thermodynamic structure within the upper ocean also has indirect impacts on other aspects of the ocean, such as the energy transfer between the ocean and the atmosphere, ocean stratification, and acoustic parameters. Full article
(This article belongs to the Section Physical Oceanography)
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<p>COAMPS atmospheric model domains (purple) with 18 km, 6 km, and 2 km grid spacings and COAMPS ocean model domain (red) with 0.02° grid spacing. This is also <a href="#jmse-12-01994-f001" class="html-fig">Figure 1</a> in May and Bourassa [<a href="#B19-jmse-12-01994" class="html-bibr">19</a>].</p>
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<p>Wintertime seasonal (including December, January, and February) means over the Gulf Stream region for the a2o2 (<b>left</b>), a2o2-cfb (<b>middle</b>), and the difference between the a2o2-cfb and a2o2 (<b>right</b>) model simulations. The top row shows surface wind stress (shaded) and surface stress vectors (arrows), the middle row shows sea surface temperature (shaded) and vector ocean surface currents (arrows), and the bottom row shows sea surface salinity. The wintertime seasonal mean surface current &gt; 1.0 m s<sup>−1</sup> is contoured in white. The seasonal mean values are included in the top left of the panels. The differences in wind stress magnitude, SST, and salinity have very similar spatial patterns, although there are notable differences in each.</p>
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<p>Vertical cross-section of the wintertime seasonal mean ocean temperature (<b>top</b>) and ocean salinity (<b>bottom</b>) across the Gulf Stream extension at 72°W for the a2o2 (<b>left</b>), a2o2-cfb (<b>middle</b>), and the a2o2-cfb minus a2o2 (<b>right</b>) model simulation. The MLD is shown with the black line. Ocean vorticity (right only) is contoured at +/− 0.00001 s<sup>−1</sup>. The maximum current within the Gulf Stream extension along 72° W is depicted with the solid gray line. The viewpoint is from upstream, meaning north of the Gulf Stream extension is to the left (negative distance) and south of the Gulf Stream extension is to the right (positive distance) of the maximum current. The spatial patterns of salinity changes due to current feedback match patterns of temperature changes, larger scale relative vorticity, and the implied vertical motion due to this larger scale relative vorticity.</p>
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<p>Wintertime seasonal means of mixed layer depth over the Gulf Stream region for the a2o2 (<b>left</b>), a2o2-cfb (<b>middle</b>), and the difference between the a2o2-cfb and a2o2 (<b>right</b>) model simulations. The seasonal mean mixed layer depth is included in the top left of the panels.</p>
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<p>Vertical cross-section of the wintertime seasonal mean ocean density across the Gulf Stream extension at 72° W for the a2o2 (<b>left</b>), a2o2-cfb (<b>middle</b>), and the a2o2-cfb minus a2o2 (<b>right</b>) model simulation. The MLD is shown with the black lines. Ocean vorticity (right only) is contoured at +/− 0.00001 s<sup>−1</sup>. The maximum current within the Gulf Stream extension along 72° W is depicted with the solid gray line. The viewpoint is upstream, meaning north of the Gulf Stream extension is to the left (negative distance) and south of the Gulf Stream extension is to the right (positive distance) of the maximum current.</p>
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<p>As in <a href="#jmse-12-01994-f004" class="html-fig">Figure 4</a>, but for ocean heat content rate of change.</p>
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<p>Wintertime seasonal mean of the rate of change in mixed layer heat budget across the Gulf Stream extension at 72° W for the a2o2 (<b>top left</b>), a2o2-cfb (<b>top middle</b>), and the a2o2-cfb minus a2o2 (<b>top right</b>) model simulation; and for the mixed layer temperature gradient (<b>bottom left</b>) and surface current Laplacian (<b>bottom right</b>). The maximum current within the Gulf Stream extension along 72° W is depicted with the solid gray line. The viewpoint is upstream, meaning north of the Gulf Stream extension is to the left (negative distance) and south of the Gulf Stream extension is to the right (positive distance) of the maximum current.</p>
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<p>Six-day mean (15 to 20 January 2016) surface current (<b>top</b>) over the Gulf Stream region for the a2o2 (<b>left</b>) and a2o2-cfb (<b>right</b>) simulations. Mean surface current &gt; 1.0 m s<sup>−1</sup> is contoured in white. Select regions north (between 39° and 40° N and 71° to 72° W) and south (35.5° to 36.5° N and 72° to 73° W) of the Gulf Stream extension are shown with black boxes. PDFs of hourly mixed layer temperature advection (°C day<sup>−1</sup>) binned by mixed layer temperature gradient in mixed layer current direction (shown by the legend in units of °C m<sup>−1</sup>) from 15 to 20 January 2016 within the defined area north of the Gulf Stream extension (<b>middle</b>) and south of the Gulf Stream extension (<b>bottom</b>). Current feedback has a much greater impact on temperature gradients (in the current direction) on the north side of the Gulf Stream extension compared to the south side.</p>
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<p>As in <a href="#jmse-12-01994-f007" class="html-fig">Figure 7</a>, but for vertical entrainment.</p>
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<p>Wintertime seasonal mean of the SST minus the mixed layer temperature across the Gulf Stream extension at 72° W for the a2o2 (blue) and the a2o2-cfb (red) model simulations (<b>left</b>), and the difference between the two simulations (<b>right</b>). The maximum current within the Gulf Stream extension along 72° W is depicted with the solid gray line. The viewpoint is upstream, meaning north of the Gulf Stream extension is to the left (negative distance) and south of the Gulf Stream extension is to the right (positive distance) of the maximum current.</p>
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<p>As in <a href="#jmse-12-01994-f004" class="html-fig">Figure 4</a>, but for submesoscale vertical heat flux at 40 m depth.</p>
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<p>As in <a href="#jmse-12-01994-f005" class="html-fig">Figure 5</a>, but for submesoscale vertical heat flux.</p>
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<p>Power spectral density of submesoscale vertical heat flux at 40 m depth averaged over 15 days (1–15 January 2016) along 39° N (<b>top</b>) and 36° N (<b>bottom</b>) for the a2o2 and the a2o2-cfb model simulations.</p>
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15 pages, 823 KiB  
Article
Acoustic Drift: Generating Helicity and Transferring Energy
by Andrey Morgulis
Axioms 2024, 13(11), 767; https://doi.org/10.3390/axioms13110767 - 4 Nov 2024
Viewed by 623
Abstract
This article studies the general properties of the Stokes drift field. This name is commonly used for the correction added to the mean Eulerian velocity for describing the averaged transport of the material particles by the oscillating fluid flows. Stokes drift is widely [...] Read more.
This article studies the general properties of the Stokes drift field. This name is commonly used for the correction added to the mean Eulerian velocity for describing the averaged transport of the material particles by the oscillating fluid flows. Stokes drift is widely known mainly in connection with another feature of oscillating flows known as steady streaming, which has been and remains the focus of a multitude of studies. However, almost nothing is known about Stokes drift in general, e.g., about its energy or helicity (Hopf’s invariant). We address these quantities for acoustic drift driven by simple sound waves with finite discrete Fourier spectra. The results discover that the mean drift energy is partly localized on a certain resonant set, which we have described explicitly. Moreover, the mean drift helicity turns out to be completely localized on the same set. We also present several simple examples to discover the effect of the power spectrum and positioning of the spectral atoms. It is revealed that tuning them can drastically change both resonant and non-resonant energies, zero the helicity, or even increase it unboundedly. Full article
(This article belongs to the Special Issue Fluid Dynamics: Mathematics and Numerical Experiment)
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<p>This figure illustrates the drift energy that arises from configuration (<a href="#FD26-axioms-13-00767" class="html-disp-formula">26</a>)–(<a href="#FD29-axioms-13-00767" class="html-disp-formula">29</a>) when the number of atoms tends to <span class="html-italic">∞</span> along a sequence of the doubled primes. The distribution of power spectrum over the atoms is the normal periodic one (right panel) or the uniform one (left panel). The graphs depict the total mean drift energy and its resonant or non-resonant fractions vs. the geometric parameter <math display="inline"><semantics> <mi>β</mi> </semantics></math>. Recall that the drift includes no uniform component for the uniform power spectrum distribution (see Remark 1).</p>
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<p>This figure displays samples of 20 level sets of the stream function (<a href="#FD59-axioms-13-00767" class="html-disp-formula">59</a>) for the drift field emergent from 22 atoms configuration defined by equalities (<a href="#FD26-axioms-13-00767" class="html-disp-formula">26</a>)–(<a href="#FD29-axioms-13-00767" class="html-disp-formula">29</a>) for equal amplitudes, <math display="inline"><semantics> <msub> <mi>φ</mi> <mi>j</mi> </msub> </semantics></math>, and <math display="inline"><semantics> <mrow> <mi>β</mi> <mo>=</mo> <mi>π</mi> <mo>/</mo> <mn>10</mn> </mrow> </semantics></math>. Upper-left, upper-right, lower-left, and lower-right frames display the samples taken for <math display="inline"><semantics> <mrow> <mi>z</mi> <mo>=</mo> <mn>0</mn> <mo>,</mo> <mn>1.69</mn> <mo>,</mo> <mn>3.38</mn> <mo>,</mo> <mn>5.08</mn> </mrow> </semantics></math>, correspondingly. So, the sampling interval is approximately eight times smaller then the period. The next semi-period demonstrates the reverse changes.</p>
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24 pages, 10209 KiB  
Article
A Simulation Study on the Effect of Supersonic Ultrasonic Acoustic Streaming on Solidification Dendrite Growth Behavior During Laser Cladding Based on Boundary Coupling
by Xing Han, Hao Zhan, Chang Li, Xuan Wang, Jiabo Liu, Shuchao Li, Qian Sun and Fanhong Kong
Coatings 2024, 14(11), 1381; https://doi.org/10.3390/coatings14111381 - 30 Oct 2024
Viewed by 622
Abstract
Laser cladding has unique technical advantages, such as precise heat input control, excellent coating properties, and local selective cladding for complex shape parts, which is a vital branch of surface engineering. During the laser cladding process, the parts are subjected to extreme thermal [...] Read more.
Laser cladding has unique technical advantages, such as precise heat input control, excellent coating properties, and local selective cladding for complex shape parts, which is a vital branch of surface engineering. During the laser cladding process, the parts are subjected to extreme thermal gradients, leading to the formation of micro-defects such as cracks, pores, and segregation. These defects compromise the serviceability of the components. Ultrasonic vibration can produce thermal, mechanical, cavitation, and acoustic flow effects in the melt pool, which can comprehensively affect the formation and evolution for the microstructure of the melt pool and reduce the microscopic defects of the cladding layer. In this paper, the coupling model of temperature and flow field for the laser cladding of 45 steel 316L was established. The transient evolution laws of temperature and flow field under ultrasonic vibration were revealed from a macroscopic point of view. Based on the phase field method, a numerical model of dendrite growth during laser cladding solidification under ultrasonic vibration was established. The mechanism of the effect of ultrasonic vibration on the solidification dendrite growth during laser cladding was revealed on a mesoscopic scale. Based on the microstructure evolution model of the paste region in the scanning direction of the cladding pool, the effects of a static flow field and acoustic flow on dendrite growth were investigated. The results show that the melt flow changes the heat and mass transfer behaviors at the solidification interface, concurrently changing the dendrites’ growth morphology. The acoustic streaming effect increases the flow velocity of the melt pool, which increases the tilt angle of the dendrites to the flow-on side and promotes the growth of secondary dendrite arms on the flow-on side. It improves the solute distribution in the melt pool and reduces elemental segregation. Full article
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<p>Coaxial laser cladding: (<b>a</b>) physical drawings for laser cladding and (<b>b</b>) schematic of laser cladding process.</p>
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<p>Temperature change physical property parameter curves for 45 steel and 316L. (<b>a</b>) Young’s modulus for 45 steel and 316L; (<b>b</b>) Poisson’s ratio of 45 steel and 316L; (<b>c</b>) density of 45 steel and 316L; (<b>d</b>) heat conductivity of 45 steel and 316L; (<b>e</b>) specific heat capacity of 45 steel and 316L; (<b>f</b>) coefficient of thermal expansion for 45 steel and 316L.</p>
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<p>Cloud image for temperature field distribution at different moments of laser cladding 316L powder on 45 steel. (<b>a</b>) Temperature field distribution at 0.3 s; (<b>b</b>) temperature field distribution at 1.0 s; (<b>c</b>) temperature field distribution at 2.0 s; (<b>d</b>) temperature field distribution at 3.0 s.</p>
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<p>Temperature boundary selection in solidification microstructure simulation. (<b>a</b>) Temperature field boundary selection for longitudinal section; (<b>b</b>) temperature field boundary selection for cross-section.</p>
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<p>Velocity distribution cloud image at different times. (<b>a</b>) Velocity distribution at 0.3 s; (<b>b</b>) velocity distribution at 1.0 s; (<b>c</b>) velocity distribution at 2.0 s; (<b>d</b>) velocity distribution at 3.0 s.</p>
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<p>Velocity distribution cloud image at different times. (<b>a</b>) Velocity distribution at 0.3 s; (<b>b</b>) velocity distribution at 1.0 s; (<b>c</b>) velocity distribution at 2.0 s; (<b>d</b>) velocity distribution at 3.0 s.</p>
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<p>Distribution cloud image for the flow field in the melt pool at 2.0 s. (<b>a</b>) Temperature distribution on the surface of the melt pool; (<b>b</b>) temperature distribution inside the melt pool.</p>
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<p>The position of the flow field collection line at 2.0 s.</p>
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<p>Static flow velocity and dimensionless flow velocity. (<b>a</b>) Velocity of static flow field; (<b>b</b>) dimensionless velocity of static flow field.</p>
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<p>Flow field distribution cloud image under action of ultrasonic flow. (<b>a</b>) Velocity distribution at 0.3 s; (<b>b</b>) velocity distribution at 2.0 s.</p>
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<p>The acoustic flow field acquisition line position at 2.0 s.</p>
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<p>Static flow velocity and dimensionless flow velocity under action of acoustic streaming. (<b>a</b>) Velocity of sound flow field; (<b>b</b>) dimensionless velocity of acoustic flow field.</p>
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<p>Dendrite growth process on laser cladding longitudinal section. (<b>a</b>) Dendrite morphology at 10 Δ<span class="html-italic">t</span>; (<b>b</b>) dendrite morphology at 1000 Δ<span class="html-italic">t</span>; (<b>c</b>) dendrite morphology at 2000 Δ<span class="html-italic">t</span>; (<b>d</b>) dendrite morphology at 3500 Δ<span class="html-italic">t</span>.</p>
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<p>Solute field morphology on laser cladding longitudinal section. (<b>a</b>) Solute field morphology at 1000 Δ<span class="html-italic">t</span>; (<b>b</b>) solute field morphology at 3500 Δ<span class="html-italic">t</span>.</p>
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<p>Dendrite morphology under static flow field. (<b>a</b>) Dendrite morphology at 2000 Δ<span class="html-italic">t</span>; (<b>b</b>) dendrite morphology at 3500 Δ<span class="html-italic">t</span>.</p>
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<p>Solute distribution with and without flow field. (<b>a</b>) Morphology of solute field without flow field; (<b>b</b>) solute field morphology in static flow field.</p>
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<p>Dendrite morphology under static acoustic streaming field. (<b>a</b>) Dendrite morphology at 2000 Δ<span class="html-italic">t</span>; (<b>b</b>) dendrite morphology at 3500 Δ<span class="html-italic">t</span>.</p>
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<p>Dendrite tilt angle under the action of flow field. (<b>a</b>) Dendrite tilt angle under static flow field; (<b>b</b>) dendrite tilt angle under static acoustic flow field.</p>
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<p>Cladding layer microstructure.</p>
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<p>Solute segregation and enrichment under static and acoustic flow fields. (<b>a</b>) Solute precipitation in flow field; (<b>b</b>) solute precipitation in acoustic flow field.</p>
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14 pages, 6575 KiB  
Article
Enhanced Acoustic Mixing in Silicon-Based Chips with Sharp-Edged Micro-Structures
by Mehrnaz Hashemiesfahan, Pierre Gelin, Han Gardeniers and Wim De Malsche
Micro 2024, 4(4), 585-598; https://doi.org/10.3390/micro4040036 - 20 Oct 2024
Viewed by 872
Abstract
The small dimensions of microfluidic channels allow for fast diffusive or passive mixing, which is beneficial for time-sensitive applications such as chemical reactions, biological assays, and the transport of to-be-detected species to sensors. In microfluidics, the need for fast mixing within milliseconds arises [...] Read more.
The small dimensions of microfluidic channels allow for fast diffusive or passive mixing, which is beneficial for time-sensitive applications such as chemical reactions, biological assays, and the transport of to-be-detected species to sensors. In microfluidics, the need for fast mixing within milliseconds arises primarily because these devices are often used in fields where rapid and efficient mixing significantly impacts the performance and outcome of the processes. Active mixing with acoustics in microfluidic devices involves using acoustic waves to enhance the mixing of fluids within microchannels. Using sharp corners and wall patterns in acoustofluidic devices significantly enhances the mixing by acoustic streaming around these features. The streaming patterns around the sharp edges are particularly effective for the mixing because they can produce strong lateral flows that rapidly homogenize liquids. This work presents extensive characterizations of the effect of sharp-edged structures on acoustic mixing in bulk acoustic wave (BAW) mode in a silicon microdevice. The effect of side wall patterns in different angles and shapes, their positions, the type of piezoelectric transducer, and its amplitude and frequency have been studied. Following the patterning of the channel walls, a mixing time of 25 times faster was reached, compared to channels with smooth side walls exhibiting conventional BAW behavior. The average locally determined acoustic streaming velocity inside the channel becomes 14 times faster if sharp corners of 10° are added to the wall. Full article
(This article belongs to the Section Analysis Methods and Instruments)
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<p>(<b>a</b>) The acoustofluidic setup schematic, including the microchip and PZT transducer, is fixed in a PMMA holder. (<b>b</b>) The schematics of the different device designs used: (device a) Microdevice with periodic 30° sharp edge; (device b) Microdevice with 10°, 20°, 30°, 40°, 50°, and 60°sharp edge; (device c) Microdevice with sharp corners with various tip shapes; (device d) Microdevice with triangular pillars in the middle of the channel; (device e) Microdevice with circular pillars amid the channel.</p>
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<p>A SEM image of the sharp corners etched alongside the silicon microfluidic channel in device a.</p>
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<p>The resulting streaming velocity for a range of PZT devices and applied frequencies. The experiments for each condition were repeated three times, and the movies were recorded. For each movie, a random number between 15 and 25 particles was tracked, and the average streaming velocity was indicated. The error bars are twice the standard deviation of the three average streaming velocities.</p>
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<p>The mixing efficiency experiments and a graph representing the results. The top image shows a continuous flow of water in the middle and fluorescent dye from both sides when the acoustics are off. The bottom image is when the acoustics have turned on, and the water and fluorescent dye are mixed. The graph extracted from MATLAB shows that the mixing efficiency reached almost 80% in 0.2 s.</p>
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<p>The velocity vectors (arrows in red) of the acoustic streaming around the sharp edges on the side wall of the silicon channel (device a) when 7 V (<b>left</b>) and 20 V (<b>right</b>) voltage are applied. Please refer to <a href="#app1-micro-04-00036" class="html-app">SI (SI)</a>, <a href="#app1-micro-04-00036" class="html-app">S1</a> (7 V), and <a href="#app1-micro-04-00036" class="html-app">S2</a> (20 V) for the recorded <a href="#app1-micro-04-00036" class="html-app">experimental video</a>.</p>
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<p>The effect of different angles of sharp corners (device b) on the average velocity magnitude. The images are taken from the chip from the top with an optical microscope. The channels with 10°, 20°, and (30°, 40°, and 60°) result in 14, 8, and 1.5 times faster streaming consecutively compared to a straight channel with the same width and depth at 28 V.</p>
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<p>(<b>a</b>–<b>d</b>) The z-stacking of 1 µm polystyrene particles movement along the acoustic streaming around the sharp corners with numerous tip shapes. The tip shapes shown in green are the initially designed tip and the above image of them is taken with an optical microscope after the device has been fabricated.</p>
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<p>A column graph of the effect of sharp tip and analyzed area on the average velocity magnitude. The blue bars are the measured average velocity in a 2.5 times bigger area (blue dashed lines) and measured average velocity in the smaller area (dashed green lines) are depicted as green bars.</p>
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<p>The z-stacking of the particle movements in the channel of device d with triangular pillars. The top-left image shows all the frames since the start of streaming and pumping on top of one another.</p>
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<p>(<b>a</b>) The z-stacking of particle movements in the channel of device e with circular pillars. The top-left image is all the frames since the start of streaming and pumping on top of each other. (<b>b</b>) A cross-section of an etched feature showing the scallop formation that causes circulation in the circular pillars (number 1 in the figure is 0.80 µm and number 2 is 3.33 µm).</p>
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<p>(<b>a</b>) Before the pumping starts, liquid movement patterns form inside the channel around each pillar, which increases with an increase in amplitude. The flow velocity in the channel with triangular pillars is higher than that with circular pillars. (<b>b</b>) After the pumping effect starts, the pumping velocity increases with time. This increase is more significant in the channel with triangular pillars.</p>
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16 pages, 3085 KiB  
Article
Theoretical and Experimental Assessment of Nonlinear Acoustic Effects through an Orifice
by Elio Di Giulio, Riccardo Di Leva and Raffaele Dragonetti
Acoustics 2024, 6(4), 818-833; https://doi.org/10.3390/acoustics6040046 - 30 Sep 2024
Viewed by 1398
Abstract
Nonlinear acoustic effects become prominent when acoustic waves propagate through an orifice, particularly at higher pressure amplitudes, potentially generating vortex rings and transferring acoustic energy into the flow. This study develops and validates a predictive theoretical model for acoustic behaviour both within and [...] Read more.
Nonlinear acoustic effects become prominent when acoustic waves propagate through an orifice, particularly at higher pressure amplitudes, potentially generating vortex rings and transferring acoustic energy into the flow. This study develops and validates a predictive theoretical model for acoustic behaviour both within and outside an orifice under linear conditions. Using transfer matrices, the model predicts the external acoustic field, while finite element numerical simulations are employed to validate the theoretical predictions in the linear regime. The experimental setup includes an impedance tube with a plate and orifice, supported by a custom-built system, where a loudspeaker generates acoustic waves. A single microphone is used to measure acoustic particle velocity and characterize the phenomenon, enabling the identification of the onset of nonlinearity. The experimental data show good agreement with the linear theoretical predictions. This work represents the first observation of nonlinear effects in a free-field environment within a semi-anechoic chamber, eliminating reflections from external surfaces, and demonstrates the efficacy of a purely acoustic-based system (speaker and two microphones) for evaluating speaker velocity and the resulting velocity within the orifice. Full article
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<p>Frequency Phase diagrams developed by Ingård [<a href="#B27-acoustics-06-00046" class="html-bibr">27</a>] for an orifice with 0.05 cm thickness and a diameter of (<b>a</b>) 0.5 cm and (<b>b</b>) 1.0 cm.</p>
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<p>Schematic representation of the experimental setup in a semi-anechoic chamber. The setup includes a speaker emitting sound waves into a plane wave tube with a perforated plate at the end. Two microphones are positioned within the setup: one for measuring the volume velocity of the speaker and the other for detecting acoustic pressure at a specific point in the external field.</p>
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<p>The flange and plate with the orifice.</p>
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<p>Experimental setup placed in the semi-anechoic chamber; microphone placed 45 cm from the orifice.</p>
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<p>Loudspeaker setup including its back cavity and an internal microphone. The microphone is positioned inside the back cavity to measure the acoustic pressure necessary for determining the speaker’s velocity.</p>
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<p>Computational Domain: in light blue, the lossless region, in red the thermoviscous region corresponding to the orifice and its inlet and outlet near region (zoomed section on the left), in light orange the Perfectly Matched Layer non-reflecting domain.</p>
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<p>Mesh used in the numerical simulations. On the left, the refined grid of the narrow region of the orifice is highlighted.</p>
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<p>On the (<b>left</b>), the colormap of the acoustic velocity near the orifice region. On the (<b>right</b>), the colormap of the acoustic pressure all over the fluid domain.</p>
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<p>Comparison between numerical simulations and the Transfer Matrix Approach reported in terms of polar plot of the acoustic pressure at a distance of 1 m from the orifice.</p>
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<p>Comparison between numerical simulations and the Transfer Matrix Approach reported in terms of acoustic pressure for the same angle (90°) at different distances from the orifice.</p>
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<p>Comparison between numerical simulations and the Transfer Matrix Approach reported in terms of Sound Pressure Level (1 m, 90°) against the frequency axis.</p>
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<p>Experimental acoustic pressure in the speaker back cavity against the Voltage Gain.</p>
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<p>Error plot showing the mean and standard deviation of measurements repeated four times for each frequency. The experimental results report the acoustic pressure against the acoustic velocity in the orifice.</p>
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<p>Frequency response of the speaker’s back cavity showing the resonance peak.</p>
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18 pages, 4081 KiB  
Article
A Dual-Stream Deep Learning-Based Acoustic Denoising Model to Enhance Underwater Information Perception
by Wei Gao, Yining Liu and Desheng Chen
Remote Sens. 2024, 16(17), 3325; https://doi.org/10.3390/rs16173325 - 8 Sep 2024
Viewed by 3766
Abstract
Estimating the line spectra of ship-radiated noise is a crucial remote sensing technique for detecting and recognizing underwater acoustic targets. Improving the signal-to-noise ratio (SNR) makes the low-frequency components of the target signal more prominent. This enhancement aids in the detection of underwater [...] Read more.
Estimating the line spectra of ship-radiated noise is a crucial remote sensing technique for detecting and recognizing underwater acoustic targets. Improving the signal-to-noise ratio (SNR) makes the low-frequency components of the target signal more prominent. This enhancement aids in the detection of underwater acoustic signals using sonar. Based on the characteristics of low-frequency narrow-band line spectra signals in underwater target radiated noise, we propose a dual-stream deep learning network with frequency characteristics transformation (DS_FCTNet) for line spectra estimation. The dual streams predict amplitude and phase masks separately and use an information exchange module to swap learn features between the amplitude and phase spectra, aiding in better phase information reconstruction and signal denoising. Additionally, a frequency characteristics transformation module is employed to extract convolutional features between channels, obtaining global correlations of the amplitude spectrum and enhancing the ability to learn target signal features. Through experimental analysis on ShipsEar, a dataset of underwater acoustic signals by hydrophones deployed in shallow water, the effectiveness and rationality of different modules within DS_FCTNet are verified.Under low SNR conditions and with unknown ship types, the proposed DS_FCTNet model exhibits the best line spectrum enhancement compared to methods such as SEGAN and DPT_FSNet. Specifically, SDR and SSNR are improved by 14.77 dB and 13.58 dB, respectively, enabling the detection of weaker target signals and laying the foundation for target localization and recognition applications. Full article
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<p>The T-F domain of clean signal and its mixed signal after adding noise.</p>
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<p>The PSD of clean signal and its mixed signal after adding noise.</p>
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<p>The architecture of the proposed DS_FCTNet model.</p>
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<p>The diagram of the encoder. Above is the amplitude encoding layer, and below is the phase encoding layer.</p>
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<p>The diagram of DSB, including the amplitude-stream block, phase-stream block, and communication.</p>
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<p>The diagram of FCT.</p>
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<p>The diagram of the Decoder Layer. Above is the amplitude encoding layer, and below is the phase encoding layer.</p>
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<p>The arrangement of three DSB modules.</p>
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<p>Comparison of the clean signal with the denoised signal using ablation experiments in the T-F domain.</p>
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<p>Comparison of the clean signal with the denoised signal using ablation experiments in PSD.</p>
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<p>Comparison of the clean signal with the denoised signal using methods in the T-F domain on Dataset-I.</p>
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<p>Comparison of the clean signal with the denoised signal using methods in PSD on Dataset-I.</p>
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<p>Comparison of the clean signal with the denoised signal using ablation experiments in the time domain.</p>
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<p>Comparison of the clean signal with the denoised signal using methods in the T-F domain on Dataset-II.</p>
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<p>Comparison of the clean signal with the denoised signal using methods in PSD on Dataset-II.</p>
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<p>Comparison of the clean signal with the denoised signal using methods for unknown ship types in PSD on Dataset-III.</p>
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<p>Comparison of the clean signal with the denoised signal using methods for unknown ship types in the T-F domain on Dataset-III.</p>
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24 pages, 3882 KiB  
Article
Open-Set Recognition of Pansori Rhythm Patterns Based on Audio Segmentation
by Jie You and Joonwhoan Lee
Appl. Sci. 2024, 14(16), 6893; https://doi.org/10.3390/app14166893 - 6 Aug 2024
Viewed by 817
Abstract
Pansori, a traditional Korean form of musical storytelling, is characterized by performances involving a vocalist and a drummer. It is well-known for the singer’s expressive narrative (aniri) and delicate gesture with fan in hand. The classical Pansori repertoires mostly tell love, satire, and [...] Read more.
Pansori, a traditional Korean form of musical storytelling, is characterized by performances involving a vocalist and a drummer. It is well-known for the singer’s expressive narrative (aniri) and delicate gesture with fan in hand. The classical Pansori repertoires mostly tell love, satire, and humor, as well as some social lessons. These performances, which can extend from three to five hours, necessitate that the vocalist adheres to precise rhythmic structures. The distinctive rhythms of Pansori are crucial for conveying both the narrative and musical expression effectively. This paper explores the challenge of open-set recognition, aiming to efficiently identify unknown Pansori rhythm patterns while applying the methodology to diverse acoustic datasets, such as sound events and genres. We propose a lightweight deep learning-based encoder–decoder segmentation model, which employs a 2-D log-Mel spectrogram as input for the encoder and produces a frame-based 1-D decision along the temporal axis. This segmentation approach, processing 2-D inputs to classify frame-wise rhythm patterns, proves effective in detecting unknown patterns within time-varying sound streams encountered in daily life. Throughout the training phase, both center and supervised contrastive losses, along with cross-entropy loss, are minimized. This strategy aimed to create a compact cluster structure within the feature space for known classes, thereby facilitating the recognition of unknown rhythm patterns by allocating ample space for their placement within the embedded feature space. Comprehensive experiments utilizing various datasets—including Pansori rhythm patterns (91.8%), synthetic datasets of instrument sounds (95.1%), music genres (76.9%), and sound datasets from DCASE challenges (73.0%)—demonstrate the efficacy of our proposed method to detect unknown events, as evidenced by the AUROC metrics. Full article
(This article belongs to the Special Issue Algorithmic Music and Sound Computing)
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<p>The pipeline of open-set recognition for Pansori rhythm patterns.</p>
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<p>The structure of the open-set audio-segmentation network.</p>
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<p>The difference between self-supervised contrastive learning and supervised contrastive learning.</p>
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<p>The process overview of audio segmentation-data preparation. Two are natural, and two are synthetic temporal data for the experiments.</p>
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<p>The process overview of audio-segmentation-data preparation.</p>
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<p>The visualization result of open-set pansori rhythm pattern detection.</p>
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<p>TSNE visualization results of the pansori rhythm pattern segmentation before (<b>left</b>)/after (<b>right</b>) using our proposed loss. On the right, each cluster associated with a rhythm pattern is well clumped together and separated from others.</p>
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<p>The visualization result of unknown-instrument sound detection. The audio sequences (<b>a</b>–<b>d</b>) illustrate the segmentation results, where each sequence is played on different instruments.</p>
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<p>The visualization result of the temporal GTZAN dataset. The sequences (<b>a</b>–<b>e</b>) illustrate the segmentation results, with each sequence mixing different styles.</p>
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<p>The visualization result of the sound event-detection dataset.</p>
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20 pages, 7336 KiB  
Article
Spectral Features Analysis for Print Quality Prediction in Additive Manufacturing: An Acoustics-Based Approach
by Michael Olowe, Michael Ogunsanya, Brian Best, Yousef Hanif, Saurabh Bajaj, Varalakshmi Vakkalagadda, Olukayode Fatoki and Salil Desai
Sensors 2024, 24(15), 4864; https://doi.org/10.3390/s24154864 - 26 Jul 2024
Cited by 2 | Viewed by 950
Abstract
Quality prediction in additive manufacturing (AM) processes is crucial, particularly in high-risk manufacturing sectors like aerospace, biomedicals, and automotive. Acoustic sensors have emerged as valuable tools for detecting variations in print patterns by analyzing signatures and extracting distinctive features. This study focuses on [...] Read more.
Quality prediction in additive manufacturing (AM) processes is crucial, particularly in high-risk manufacturing sectors like aerospace, biomedicals, and automotive. Acoustic sensors have emerged as valuable tools for detecting variations in print patterns by analyzing signatures and extracting distinctive features. This study focuses on the collection, preprocessing, and analysis of acoustic data streams from a Fused Deposition Modeling (FDM) 3D-printed sample cube (10 mm × 10 mm × 5 mm). Time and frequency-domain features were extracted at 10-s intervals at varying layer thicknesses. The audio samples were preprocessed using the Harmonic–Percussive Source Separation (HPSS) method, and the analysis of time and frequency features was performed using the Librosa module. Feature importance analysis was conducted, and machine learning (ML) prediction was implemented using eight different classifier algorithms (K-Nearest Neighbors (KNN), Support Vector Machine (SVM), Gaussian Naive Bayes (GNB), Decision Trees (DT), Logistic Regression (LR), Random Forest (RF), Extreme Gradient Boosting (XGB), and Light Gradient Boosting Machine (LightGBM)) for the classification of print quality based on the labeled datasets. Three-dimensional-printed samples with varying layer thicknesses, representing two print quality levels, were used to generate audio samples. The extracted spectral features from these audio samples served as input variables for the supervised ML algorithms to predict print quality. The investigation revealed that the mean of the spectral flatness, spectral centroid, power spectral density, and RMS energy were the most critical acoustic features. Prediction metrics, including accuracy scores, F-1 scores, recall, precision, and ROC/AUC, were utilized to evaluate the models. The extreme gradient boosting algorithm stood out as the top model, attaining a prediction accuracy of 91.3%, precision of 88.8%, recall of 92.9%, F-1 score of 90.8%, and AUC of 96.3%. This research lays the foundation for acoustic based quality prediction and control of 3D printed parts using Fused Deposition Modeling and can be extended to other additive manufacturing techniques. Full article
(This article belongs to the Collection Sensors and Sensing Technology for Industry 4.0)
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<p>Schematic of the acoustic sensor experimental set-up.</p>
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<p>Image showing printed samples of varying layer thickness.</p>
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<p>The schematic of the HPSS algorithm.</p>
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<p>Typical machine learning steps for classification.</p>
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<p>Visual representation of the harmonic and percussive segments of an AM sound signal.</p>
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<p>RMS energy vs frame index of a 10-s audio segment of AM sound signals.</p>
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<p>Spectral roll-off vs frame index of a 10-s audio segment of AM sound signals.</p>
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<p>Amplitude vs time comparison of raw audio and denoised audio (spectral subtraction and HPSS).</p>
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<p>Feature ranking of the spectral features.</p>
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<p>Correlation matrix of the spectral features.</p>
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<p>Confusion matrix of the LR, GNB, DT, and LightGBM algorithms.</p>
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<p>Confusion matrix of the KNN, SVM, RF, and XGB algorithms.</p>
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<p>The bar chart of the performance metrics for all the eight classifiers.</p>
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<p>AUCROC and AUPRC for the eight classification algorithms.</p>
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17 pages, 4312 KiB  
Article
Photon-Induced Photo-Acoustic Streaming vs. Shock Wave-Enhanced Emission Photo-Acoustic Streaming—The Effect of Three Final Irrigation Protocols on the Bond Strength of an Individually Formed Fiber Post
by Cassandra Lupita, Daliana Emanuela Bojoga, Alessandro Del Vecchio, Dan Ioan Stoia, Ion Grozav, Mariana Ioana Miron and Darinca Carmen Todea
Dent. J. 2024, 12(8), 237; https://doi.org/10.3390/dj12080237 - 26 Jul 2024
Viewed by 900
Abstract
(1) Background: This study aimed to evaluate how laser-activated irrigation (LAI) influences the retention of a fiber post when used before an endodontic filling, as well as after post space preparation. (2) Materials and Methods: Sixty freshly extracted human incisors were selected. The [...] Read more.
(1) Background: This study aimed to evaluate how laser-activated irrigation (LAI) influences the retention of a fiber post when used before an endodontic filling, as well as after post space preparation. (2) Materials and Methods: Sixty freshly extracted human incisors were selected. The teeth were randomly assigned to three groups—CONVENTIONAL (CONV), PIPS or SWEEPS—and treated endodontically. Each group received irrigation with 1 × 5 mL EDTA (17%) and 3 × 5 mL NaOCl (5.25%). In the first group, the irrigants were not activated, while in the second and third group, LAI was adopted using PIPS and SWEEPS protocols (Lightwalker from Fotona, Ljubliana, Slovenia). After post space preparation, each group received the same irrigation protocol initially established. Sticky posts (everStick Post, GC AUSTRIA GmbH Swiss) were individually adapted to the corresponding post spaces and cemented using dual cure resin cement (Gradia Core, GC Austria GmbH Swiss). All specimens were vertically embedded into self-curing acrylate (Duracryl plus, Spofa Dent, Europe), and each was sectioned into three segments of type A and type B samples for debonding through push-out and pull-out tests. The results were statistically analyzed. (3) Results: The pull-out test showed the superiority of the SWEEPS group, with a mean fracture force of 133.0 ± 50.7 N, followed by the PIPS group, with 102 N, with a lower standard deviation of ± 34.5 N. The CONV group registered the lowest fracture force. Concerning the push-out test, the SWEEPS group showed superior shear stress in comparison to the other two groups (13.45 ± 4.29 MPa); the CONV group was inferior, with shear tension values of 8.31 ± 4.67 MPa. (4) Conclusions: It can be stated that the SWEEPS and PIPS protocols resulted in considerably higher fiber post retention than the conventional method, whereas the SWEEPS protocol was superior to the PIPS protocol. Full article
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<p>The sectioned parts of the root considered in this study.</p>
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<p>The aspects of sample types A and B for all 3 groups.</p>
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<p>The scheme of sample loading: (<b>a</b>) sample mounting into the fixing device; (<b>b</b>) sample gripping, ready for test.</p>
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<p>The type B sample loading: (<b>a</b>) sample sustaining piece; (<b>b</b>) testing equipment.</p>
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<p>The sample breaking by pulling: (<b>a</b>) PIPS group; (<b>b</b>) SWEEPS group; (<b>c</b>) CONV group.</p>
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<p>Statistical results of the pull-out test for Type A samples in the CONV, PIPS, and SWEEPS groups.</p>
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<p>Sample failures due to pushing of the fiber post: (<b>a</b>) PIPS group; (<b>b</b>) SWEEPS group; (<b>c</b>) CONV. group.</p>
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<p>The characteristic force–displacement curves of the CONV, PIPS, and SWEEPS groups.</p>
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<p>Chart of the mean and standard deviation of shear stress.</p>
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<p>Graphical results of the pull-out test for Type B samples in the CONV, PIPS, and SWEEPS groups.</p>
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23 pages, 4933 KiB  
Article
Advanced Multimodal Sentiment Analysis with Enhanced Contextual Fusion and Robustness (AMSA-ECFR): Symmetry in Feature Integration and Data Alignment
by Qing Chen, Shenghong Dong and Pengming Wang
Symmetry 2024, 16(7), 934; https://doi.org/10.3390/sym16070934 - 22 Jul 2024
Viewed by 2317
Abstract
Multimodal sentiment analysis, a significant challenge in artificial intelligence, necessitates the integration of various data modalities for accurate human emotion interpretation. This study introduces the Advanced Multimodal Sentiment Analysis with Enhanced Contextual Fusion and Robustness (AMSA-ECFR) framework, addressing the critical challenge of data [...] Read more.
Multimodal sentiment analysis, a significant challenge in artificial intelligence, necessitates the integration of various data modalities for accurate human emotion interpretation. This study introduces the Advanced Multimodal Sentiment Analysis with Enhanced Contextual Fusion and Robustness (AMSA-ECFR) framework, addressing the critical challenge of data sparsity in multimodal sentiment analysis. The main components of the proposed approach include a Transformer-based model employing BERT for deep semantic analysis of textual data, coupled with a Long Short-Term Memory (LSTM) network for encoding temporal acoustic features. Innovations in AMSA-ECFR encompass advanced feature encoding for temporal dynamics and an adaptive attention-based model for efficient cross-modal integration, achieving symmetry in the fusion and alignment of asynchronous multimodal data streams. Additionally, the framework employs generative models for intelligent approximation of missing features. It ensures robust alignment of high-level features with multimodal data context, effectively tackling issues of incomplete or noisy inputs. In simulation studies, the AMSA-ECFR model demonstrated superior performance against existing approaches. The symmetrical approach to feature integration and data alignment contributed significantly to the model’s robustness and precision. In simulations, the AMSA-ECFR model demonstrated a 10% higher accuracy and a 15% lower mean absolute error than the current best multimodal sentiment analysis frameworks. Full article
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<p>Conceptual representation of AMSA-ECFR’s approach to overcoming traditional MSA challenges.</p>
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<p>AMSA-ECFR framework: an integrative architecture for robust Multimodal Sentiment Analysis featuring advanced feature encoding, dynamic cross-modal interaction, and context-aware reconstruction.</p>
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<p>Comparative performance analysis of Multimodal Sentiment Analysis frameworks over increasing missing data rates, highlighting the proposed model’s superior resilience and predictive accuracy.</p>
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<p>Performance metrics of Multimodal Sentiment Analysis frameworks as a function of increasing missing data rates, demonstrating the proposed model’s enduring accuracy and correlation with ground truth sentiment.</p>
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<p>Efficacy of Multimodal Sentiment Analysis frameworks in conditions of varied missing data rates, showcasing the proposed model’s consistency in MAE, CCC, and accuracy measures.</p>
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<p>Computational efficiency analysis of the AMSA-ECFR framework.</p>
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<p>Synchronized Multimodal Analysis depicting emotional expressions in correlation with linguistic, auditory, and visual data streams, demonstrating the complex layering of sentiment cues.</p>
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17 pages, 2937 KiB  
Article
Emotion Recognition from Videos Using Multimodal Large Language Models
by Lorenzo Vaiani, Luca Cagliero and Paolo Garza
Future Internet 2024, 16(7), 247; https://doi.org/10.3390/fi16070247 - 13 Jul 2024
Viewed by 2412
Abstract
The diffusion of Multimodal Large Language Models (MLLMs) has opened new research directions in the context of video content understanding and classification. Emotion recognition from videos aims to automatically detect human emotions such as anxiety and fear. It requires deeply elaborating multiple data [...] Read more.
The diffusion of Multimodal Large Language Models (MLLMs) has opened new research directions in the context of video content understanding and classification. Emotion recognition from videos aims to automatically detect human emotions such as anxiety and fear. It requires deeply elaborating multiple data modalities, including acoustic and visual streams. State-of-the-art approaches leverage transformer-based architectures to combine multimodal sources. However, the impressive performance of MLLMs in content retrieval and generation offers new opportunities to extend the capabilities of existing emotion recognizers. This paper explores the performance of MLLMs in the emotion recognition task in a zero-shot learning setting. Furthermore, it presents a state-of-the-art architecture extension based on MLLM content reformulation. The performance achieved on the Hume-Reaction benchmark shows that MLLMs are still unable to outperform the state-of-the-art average performance but, notably, are more effective than traditional transformers in recognizing emotions with an intensity that deviates from the average of the samples. Full article
(This article belongs to the Special Issue Generative Artificial Intelligence in Smart Societies)
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<p>Probability density function of all emotions in the dataset generated by a Gaussian Kernel Density Estimation.</p>
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<p>Sketch of the probing pipeline. Video-LLaVA produces meaningful video embeddings through token average pooling, to which a probing network is applied to predict emotion scores. The circle on the right side focuses on the internal structure of the probing network.</p>
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<p>Integration of Video-LLaVA [<a href="#B12-futureinternet-16-00247" class="html-bibr">12</a>] textual features into the state-of-the-art ViPER [<a href="#B9-futureinternet-16-00247" class="html-bibr">9</a>] architecture. First, the entire video is passed as input to the Video-LLaVA [<a href="#B12-futureinternet-16-00247" class="html-bibr">12</a>] model. This MLLM produces a unique description that is encoded and concatenated to each input token of the Perceiver module of ViPER [<a href="#B9-futureinternet-16-00247" class="html-bibr">9</a>].</p>
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<p>Integration of LLaVA textual features into the state-of-the-art ViPER [<a href="#B9-futureinternet-16-00247" class="html-bibr">9</a>] architecture. The video is sampled to extract 32 equally spaced frames, used to feed the LLaVA model. Then, it produces a different description for each frame. Finally, these descriptions are encoded and concatenated to the corresponding input token of the Perceiver module of ViPER [<a href="#B9-futureinternet-16-00247" class="html-bibr">9</a>].</p>
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<p>ViPER-VATF [<a href="#B9-futureinternet-16-00247" class="html-bibr">9</a>] based on CLIP [<a href="#B26-futureinternet-16-00247" class="html-bibr">26</a>] textual features prediction for the Adoration emotion. The average prediction is 0.3737 ± 0.0867, with a minimum prediction score of 0 and a maximum of 0.5500.</p>
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<p>ViPER-VATF [<a href="#B9-futureinternet-16-00247" class="html-bibr">9</a>] based on CLIP [<a href="#B26-futureinternet-16-00247" class="html-bibr">26</a>] textual features prediction for the Empathic Pain emotion. The average prediction is 0.2088 ± 0.0669, with a minimum prediction score of 0.0812 and a maximum of 0.5513.</p>
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<p>ViPER-VATF [<a href="#B9-futureinternet-16-00247" class="html-bibr">9</a>] based on Video-LLaVA [<a href="#B12-futureinternet-16-00247" class="html-bibr">12</a>] textual features prediction for the Adoration emotion. The average prediction is 0.3465 ± 0.1387, with a minimum score of 0 and maximum score of 0.6289.</p>
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<p>ViPER-VATF [<a href="#B9-futureinternet-16-00247" class="html-bibr">9</a>] based on Video-LLaVA [<a href="#B12-futureinternet-16-00247" class="html-bibr">12</a>] textual features prediction for the Empathic Pain emotion. The average prediction is 0.2372 ± 0.1099, with a minimum score of 0.0369 and a maximum score of 0.5848.</p>
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