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Calibration and Verification of Operation Parameters for an Array of Vectrino Profilers Configured for Turbulent Flow Field Measurement around Bridge Piers—Part II 用于桥墩周围湍流流场测量的Vectrino剖面仪阵列操作参数的校准和验证-第二部分
Q3 MECHANICS Pub Date : 2023-06-29 DOI: 10.3390/fluids8070199
Gordon Gilja, Robert Fliszar, Antonija Harasti, Manousos Valyrakis
High-frequency velocimeters used for flow measurements during laboratory experiments allow the user to select the range for several operation parameters to set up the instrument for optimal velocity measurement. The discrepancies between velocity measurements collected with different instrument configurations can be significant, depending on the flume bed configuration and boundary conditions. The aim of this paper is to quantify the differences in flow velocity profiles measured with Acoustic Doppler Velocimeter Profilers (ADVPs) configured using a combination of profiling parameters: Ping Algorithm (PA), Transmit Pulse Size (TPS), and Cell Size (CS). Whereas in Part I of this research, the goal was to identify the optimal probe configuration for downstream measurement of the complex hydraulic structure (pier protected with riprap) based on a match of the flow rate with measurements from other instruments, in this paper, effect of distinct probe configuration on velocity profile and turbulent kinetic energy (TKE) is demonstrated. Differences between ADVPs’ configurations were analyzed through sensitivity analysis with the intention to calculate and compare any discrepancies in the velocity measurements for all the three measured velocity components: streamwise u, spanwise v and vertical w collected on two characteristic flume cross-sections. The results show that each parameter change has a significant effect on the measured values of each velocity component when compared to the Target Configuration (TC). The largest root-mean-square-error (RMSE) is observed when TPS is changed, followed by CS and PA. Absolute RMSE calculated for TPS change from 4 mm to 1 mm is, on average, 6.30 cm/s, 0.90 cm/s, and 0.82 cm/s for velocity components u, v and w, respectively. Absolute RMSE calculated for CS change from 1 mm to 4 mm is, on average, 4.49 cm/s, 0.88 cm/s, and 0.71 cm/s for velocity components u, v and w, respectively. Absolute RMSE calculated for PA change from Adaptive to Max interval is, on average, 4.04 cm/s, 0.63 cm/s, and 0.68 cm/s for velocity components u, v and w, respectively. For a change in all parameters, RMSE is greater for the cross-section downstream of the pier than for the approach cross-section: on average, 90%, 57% and 54% for a change in the PA, TPS, and CS, respectively.
高频测速仪用于实验室实验期间的流量测量,允许用户选择几个操作参数的范围,以设置仪器的最佳速度测量。根据水槽结构和边界条件的不同,不同仪器配置收集的流速测量值之间的差异可能是显著的。本文的目的是量化用多普勒测速分析器(advp)测量的流速剖面的差异,这些剖面参数包括:Ping算法(PA)、传输脉冲大小(TPS)和单元大小(CS)。在本研究的第一部分中,目标是根据流量与其他仪器的测量结果相匹配,确定用于复杂水工结构(有碎石保护的桥墩)下游测量的最佳探头配置,而在本文中,不同探头配置对速度剖面和湍流动能(TKE)的影响进行了论证。通过敏感性分析分析advp配置之间的差异,目的是计算和比较在两个特征水槽截面上收集的所有三个测量速度分量:流向u,展向v和垂直w的速度测量结果的差异。结果表明,与目标配置(TC)相比,每次参数变化对各速度分量的测量值都有显著影响。TPS变化时均方根误差(RMSE)最大,CS次之,PA次之。速度分量u、v和w的TPS从4 mm到1 mm变化的绝对RMSE平均值分别为6.30 cm/s、0.90 cm/s和0.82 cm/s。速度分量u、v和w从1 mm到4 mm CS变化的绝对RMSE平均值分别为4.49 cm/s、0.88 cm/s和0.71 cm/s。速度分量u、v和w从Adaptive到Max区间PA变化的绝对RMSE均值分别为4.04 cm/s、0.63 cm/s和0.68 cm/s。对于所有参数的变化,桥墩下游截面的RMSE大于接近截面:PA、TPS和CS的变化平均分别为90%、57%和54%。
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引用次数: 0
Transition to Equilibrium and Coherent Structure in Ideal MHD Turbulence, Part 2 理想MHD湍流向平衡过渡和相干结构,第2部分
Q3 MECHANICS Pub Date : 2023-06-14 DOI: 10.3390/fluids8060181
John V. Shebalin
We continue our study of the transition of ideal, homogeneous, incompressible, magnetohydrodynamic (MHD) turbulence from non-equilibrium initial conditions to equilibrium using long-time numerical simulations on a 1283 periodic grid. A Fourier spectral transform method is used to numerically integrate the dynamical equations forward in time. The six runs that previously went to near equilibrium are here extended into equilibrium. As before, we neglect dissipation as we are primarily concerned with behavior at the largest scale where this behavior has been shown to be essentially the same for ideal and real (forced and dissipative) MHD turbulence. These six runs have various combinations of imposed rotation and mean magnetic field and represent the five cases of ideal, homogeneous, incompressible, and MHD turbulence: Case I (Run 1), with no rotation or mean field; Case II (Runs 2a and 2b), where only rotation is imposed; Case III (Run 3), which has only a mean magnetic field; Case IV (Run 4), where rotation vector and mean magnetic field direction are aligned; and Case V (Run 5), which has non-aligned rotation vector and mean field directions. Statistical mechanics predicts that dynamic Fourier coefficients are zero-mean random variables, but largest-scale coherent magnetic structures emerge and manifest themselves as Fourier coefficients with very large, quasi-steady, mean values compared to their standard deviations, i.e., there is ‘broken ergodicity.’ These magnetic coherent structures appeared in all cases during transition to near equilibrium. Here, we report that, as the runs were continued, these coherent structures remained quasi-steady and energetic only in Cases I and II, while Case IV maintained its coherent structure but at comparatively low energy. The coherent structures that appeared in transition in Cases III and V were seen to collapse as their associated runs extended into equilibrium. The creation of largest-scale, coherent magnetic structure appears to be a dynamo process inherent in ideal MHD turbulence, particularly in Cases I and II, i.e., those cases most pertinent to planets and stars. Furthermore, the statistical theory of ideal MHD turbulence has proven to apply at the largest scale, even when dissipation and forcing are included. This, along with the discovery and explanation of dynamically broken ergodicity, is essentially a solution to the ‘dynamo problem’.
我们继续研究理想的、均匀的、不可压缩的、磁流体动力学(MHD)湍流从非平衡初始条件到平衡的转变,使用1283周期网格上的长时间数值模拟。采用傅里叶谱变换方法对动力学方程进行时间正演数值积分。之前接近平衡的六次运行在这里延伸到平衡状态。和以前一样,我们忽略了耗散,因为我们主要关注的是在最大尺度上的行为,而这种行为已经被证明在理想和实际(强迫和耗散)MHD湍流中基本上是相同的。这六次运行具有施加旋转和平均磁场的不同组合,代表了理想、均匀、不可压缩和MHD湍流的五种情况:情况1(运行1),没有旋转或平均场;情况II(运行2a和2b),其中只施加旋转;情形III(运行3),只有平均磁场;情形IV (Run 4),旋转矢量与平均磁场方向对齐;Case V (Run 5),它具有不对齐的旋转矢量和平均场方向。统计力学预测,动态傅里叶系数是零均值随机变量,但最大规模的相干磁结构出现并表现为傅里叶系数,其平均值与其标准差相比非常大,准稳定,即存在“破遍历性”。这些磁相干结构在过渡到接近平衡状态的所有情况下都出现了。在这里,我们报告说,随着运行的继续,这些相干结构只在情形1和情形2中保持准稳定和能量,而情形4保持其相干结构,但能量相对较低。在案例III和案例V中,在过渡时期出现的连贯结构随着其相关运行扩展到平衡状态而崩溃。最大规模的相干磁结构的产生似乎是理想MHD湍流所固有的一个发电机过程,特别是在情况I和II中,即与行星和恒星最相关的那些情况。此外,理想MHD湍流的统计理论已被证明适用于最大尺度,即使包括耗散和强迫。这与动态破缺遍历性的发现和解释一起,本质上是“发电机问题”的解决方案。
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引用次数: 0
Numerical Modelling of Water Flashing at Sub-Atmopsheric Pressure with a Multi-Regime Approach 亚大气压下水闪动的多态数值模拟
Q3 MECHANICS Pub Date : 2023-04-28 DOI: 10.3390/fluids8050143
Clément Loiseau, Stéphane Mimouni, Didier Colmont, Stéphane Vincent
The CFD numerical study of the flash boiling phenomenon of a water film was conducted using an Euler–Euler method, and compared to the experiments on the flashing of a water film. The water film is initially heated at temperatures ranging from 34 to 74 ∘C (frim 1 to 41 ∘C superheat), and the pressure is decreased from 1 bar to 50 mbar during the experiments. This paper shows that the experiments could not be correctly modelled by a simple liquid/bubble model because of the overestimation of the drag force above the water film (in the gas/droplet region). The generalised large interface model (GLIM), however, a multi-regime approach implemented in the version 7.0 of the neptune_cfd software, is able to differentiate the water film, where liquid/bubble interactions are predominant from the gas region where gas/droplet interactions are predominant, and gives nice qualitative results. Finally, this paper shows that the interfacial heat transfer model of Berne for superheated liquids could accurately predict the evolution of the water temperature over time.
采用欧拉-欧拉方法对水膜闪蒸现象进行了CFD数值研究,并与水膜闪蒸实验进行了对比。水膜最初在34到74°C的温度下加热(从1到41°C的过热度),在实验过程中压力从1巴降至50毫巴。本文指出,由于高估了水膜上方(气/液滴区域)的阻力,用简单的液/泡模型不能正确地模拟实验。然而,广义大界面模型(GLIM),一种由7.0版本的neptune_cfd软件实现的多区域方法,能够区分水膜(其中液体/气泡相互作用占主导地位)和气体区域(其中气体/液滴相互作用占主导地位),并给出了很好的定性结果。最后,本文证明了过热液体的Berne界面传热模型可以准确地预测水温随时间的演变。
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引用次数: 0
Two-Fluid Large-Eddy Simulation of Two-Phase Flow in Air-Sparged Hydrocyclone 充气水力旋流器两相流的双流体大涡模拟
Q3 MECHANICS Pub Date : 2023-04-25 DOI: 10.3390/fluids8050139
Mustafa Bukhari, Hassan Fayed, Saad Ragab
The two-fluid (Euler–Euler) model and large-eddy simulation are used to compute the turbulent two-phase flow of air and water in a cyclonic flotation device known as an Air-Sparged Hydrocyclone (ASH). In the operation of ASH, air is injected through a porous cylindrical wall. The study considers a 48 mm diameter hydrocyclone and uses a block-structured fine mesh of 10.5 million hexagonal elements. The air-to-water injection ratio is 4, and a uniform air bubble diameter of 0.5 mm is specified. The flow field in ASH was investigated for the inlet flow rate of water of 30.6 L/min at different values of underflow exit pressure. The current simulations quantify the effects of the underflow exit pressure on the split ratio and the overall flow physics in ASH, including the distribution of the air volume fraction, water axial velocity, tangential velocity, and swirling-layer thickness. The loci of zero-axial velocity surfaces were determined for different exit pressures. The water split ratio through the overflow opening varies with underflow exit pressure as 6%, 8%, 16%, and 26% for 3, 4, 5, and 6 kPa, respectively. These results indicate that regulating the pressure at the underflow exit can be used to optimize the ASH’s performance. Turbulent energy spectra in different regions of the hydrocyclone were analyzed. Small-scale turbulence spectra at near-wall points exhibit f−4 law, where f is frequency. Whereas for points at the air-column interface, the energy spectra show an inertial subrange f−5/3 followed by a dissipative range of f−7 law.
采用双流体(欧拉-欧拉)模型和大涡模拟计算了气相水力旋流器(ASH)内空气和水的两相湍流。在ASH操作中,空气通过多孔圆柱壁注入。该研究考虑了直径48毫米的水力旋流器,并使用了由1050万个六边形单元组成的块结构细网格。注气比为4,规定均匀气泡直径为0.5 mm。以进气流速为30.6 L/min时,在不同底流出口压力值下,研究了ASH内的流场。目前的模拟量化了底流出口压力对ASH中劈裂比和整体流动物理的影响,包括空气体积分数、水轴向速度、切向速度和旋流层厚度的分布。在不同的出口压力下,确定了零轴速度面轨迹。在3、4、5、6 kPa条件下,溢流出口压力分别为6%、8%、16%、26%时,溢流口水分流率变化。结果表明,通过调节底流出口压力可以优化粉煤灰的性能。分析了旋流器不同区域的湍流能谱。近壁点的小尺度湍流谱表现为f−4规律,其中f为频率。而对于气柱界面处的点,能谱表现为惯性子范围f−5/3,耗散范围f−7定律。
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引用次数: 0
An Approximate Analytical Model of a Jet Flow with Mach Reflection and Pulsed Energy Supply at the Main Shock 具有马赫反射和主激波脉冲能量供给的射流近似解析模型
Q3 MECHANICS Pub Date : 2023-04-14 DOI: 10.3390/fluids8040132
Mikhail V. Chernyshov, Karina E. Savelova
The supersonic flow of a reactive gas mixture with Mach reflection of oblique shocks and pulsed energy supply at the Mach stem is considered within the framework of the Chapman–Jouguet theory. An approximate analytical model is proposed that quickly determines the shape and size of the shock-wave structure as well as the flow parameters in various flow regions. As an example of the application of the proposed analytical model, the “first barrel” of a highly overexpanded jet flow of an air-methane mixture with a high supersonic velocity, is studied. Flows of hydrogen–air and hydrogen–oxygen mixtures were also considered for comparison with preceding numerical results. The height of the triple point of the Mach reflection is determined in the presence of a change in the chemical composition of the mixture and an isobaric pulsed energy supply at the main shock.
在chapman - jouget理论的框架内考虑了斜激波反射马赫和马赫干处脉冲能量供应的反应气体混合物的超声速流动。提出了一种近似解析模型,可以快速确定激波结构的形状和大小以及各流区的流动参数。作为应用该分析模型的一个例子,研究了高超声速空气-甲烷混合物高度过膨胀射流的“第一桶”。为了与之前的数值结果进行比较,还考虑了氢-空气和氢-氧混合物的流动。马赫反射三相点的高度是在混合物的化学成分发生变化和主激波处有等压脉冲能量供应的情况下确定的。
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引用次数: 0
Vortex Formation Times in the Glottal Jet, Measured in a Scaled-Up Model. 声门射流中的旋涡形成时间,用一个放大模型测量。
IF 1.9 Q3 MECHANICS Pub Date : 2021-11-01 Epub Date: 2021-11-15 DOI: 10.3390/fluids6110412
Michael Krane

In this paper, the timing of vortex formation on the glottal jet is studied using previously published velocity measurements of flow through a scaled-up model of the human vocal folds. The relative timing of the pulsatile glottal jet and the instability vortices are acoustically important since they determine the harmonic and broadband content of the voice signal. Glottis exit jet velocity time series were extracted from time-resolved planar DPIV measurements. These measurements were acquired at four glottal flow speeds (u SS = 16.1-38 cm/s) and four glottis open times (T o = 5.67-23.7 s), providing a Reynolds number range Re = 4100-9700 and reduced vibration frequency f* = 0.01-0.06. Exit velocity waveforms showed temporal behavior on two time scales, one that correlates to the period of vibration and another characterized by short, sharp velocity peaks (which correlate to the passage of instability vortices through the glottis exit plane). The vortex formation time, estimated by computing the time difference between subsequent peaks, was shown to be not well-correlated from one vibration cycle to the next. The principal finding is that vortex formation time depends not only on cycle phase, but varies strongly with reduced frequency of vibration. In all cases, a strong high-frequency burst of vortex motion occurs near the end of the cycle, consistent with perceptual studies using synthesized speech.

在本文中,涡旋形成的时间在声门射流上进行了研究,使用先前发表的流速测量通过一个比例放大的人类声带模型。脉冲声门射流和不稳定涡的相对定时在声学上是重要的,因为它们决定了语音信号的谐波和宽带内容。从时间分辨平面DPIV测量中提取声门出口射流速度时间序列。这些测量是在四种声门流速(u SS = 16.1-38 cm/s)和四种声门打开时间(T o = 5.67-23.7 s)下获得的,雷诺数范围Re = 4100-9700,降低振动频率f* = 0.01-0.06。出口速度波形在两个时间尺度上表现出时间行为,一个与振动周期相关,另一个以短而尖锐的速度峰值为特征(这与通过声门出口平面的不稳定涡流有关)。通过计算后续峰值之间的时间差来估计涡的形成时间,表明在一个振动周期与下一个振动周期之间没有很好的相关性。主要发现是涡的形成时间不仅与周期相位有关,而且随着振动频率的降低而变化很大。在所有情况下,一个强烈的高频漩涡运动爆发发生在周期的末尾,与使用合成语音的感知研究一致。
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引用次数: 0
Nanoparticle Delivery in Prostate Tumors Implanted in Mice Facilitated by Either Local or Whole-Body Heating. 局部或全身加热促进小鼠前列腺肿瘤植入的纳米颗粒递送。
IF 1.9 Q3 MECHANICS Pub Date : 2021-08-01 DOI: 10.3390/fluids6080272
Qimei Gu, Lance Dockery, Marie-Christine Daniel, Charles J Bieberich, Ronghui Ma, Liang Zhu

This work discusses in vivo experiments that were performed to evaluate whether local or whole-body heating to 40 °C reduced interstitial fluid pressures (IFPs) and enhanced nanoparticle delivery to subcutaneous PC3 human prostate cancer xenograft tumors in mice. After heating, 0.2 mL of a previously developed nanofluid containing gold nanoparticles (10 mg Au/mL) was injected via the tail vein. The induced whole-body hyperthermia led to increases in tumor and mouse body blood perfusion rates of more than 50% and 25%, respectively, while the increases were much smaller in the local heating group. In the whole-body hyperthermia groups, the IFP reduction from the baseline at the tumor center immediately after heating was found to be statistically significant when compared to the control group. The 1 h of local heating group showed IFP reductions at the tumor center, while the IFPs increased in the periphery of the tumor. The intratumoral gold nanoparticle accumulation was quantified using inductively coupled plasma mass spectrometry (ICP-MS). Compared to the control group, 1 h or 4 h of experiencing whole-body hyperthermia resulted in an average increase of 51% or 67% in the gold deposition in tumors, respectively. In the 1 h of local heating group, the increase in the gold deposition was 34%. Our results suggest that 1 h of mild whole-body hyperthermia may be a cost-effective and readily implementable strategy for facilitating nanoparticle delivery to PC3 tumors in mice.

本研究讨论了在体内进行的实验,以评估局部或全身加热到40°C是否会降低间质液压力(IFPs),并增强纳米颗粒对小鼠皮下PC3人类前列腺癌异种移植肿瘤的递送。加热后,通过尾静脉注射0.2 mL先前开发的含有金纳米颗粒(10 mg Au/mL)的纳米流体。诱导的全身热疗导致肿瘤和小鼠体内血液灌注率分别增加50%和25%以上,而局部热疗组的增加幅度要小得多。在全身热疗组中,与对照组相比,加热后立即从肿瘤中心基线降低的IFP具有统计学意义。局部加热1 h时,肿瘤中心IFP降低,肿瘤周围IFP升高。采用电感耦合等离子体质谱法(ICP-MS)定量测定肿瘤内金纳米颗粒的积累。与对照组相比,全身热疗1小时或4小时导致肿瘤中的金沉积平均分别增加51%或67%。局部加热组1 h,金沉积量增加34%。我们的研究结果表明,1小时的轻度全身热疗可能是促进纳米颗粒递送到小鼠PC3肿瘤的一种经济有效且易于实施的策略。
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引用次数: 2
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Fluids
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