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System Identification Using Self-Adaptive Filtering Applied to Second-Order Gradient Materials 将自适应滤波技术应用于二阶梯度材料的系统识别技术
Pub Date : 2024-04-07 DOI: 10.3390/dynamics4020015
T. Kletschkowski
For many engineering applications, it is sufficient to use the concept of simple materials. However, higher gradients of the kinematic variables are taken into account to model materials with internal length scales as well as to describe localization effects using gradient theories in finite plasticity or fluid mechanics. In many approaches, length scale parameters have been introduced that are related to a specific micro structure. An alternative approach is possible, if a thermodynamically consistent framework is used for material modeling, as shown in the present contribution. However, even if sophisticated and thermodynamically consistent material models can be established, there are still not yet standard experiments to determine higher order material constants. In order to contribute to this ongoing discussion, system identification based on the method of self-adaptive filtering is proposed in this paper. To evaluate the effectiveness of this approach, it has been applied to second-order gradient materials considering longitudinal vibrations. Based on thermodynamically consistent models that have been solved numerically, it has been possible to prove that system identification based on self-adaptive filtering can be used effectively for both narrow-band and broadband signals in the field of second-order gradient materials. It has also been found that the differences identified for simple materials and gradient materials allow for condition monitoring and detection of gradient effects in the material behavior.
在许多工程应用中,使用简单材料的概念就足够了。然而,在使用有限塑性或流体力学中的梯度理论建立具有内部长度尺度的材料模型以及描述局部效应时,需要考虑运动变量的较高梯度。许多方法都引入了与特定微观结构相关的长度尺度参数。如果采用热力学一致的框架进行材料建模,则可以采用另一种方法,如本文所示。然而,即使可以建立复杂且热力学上一致的材料模型,仍没有标准实验来确定高阶材料常数。为了推动这一正在进行的讨论,本文提出了基于自适应滤波方法的系统识别方法。为了评估这种方法的有效性,本文将其应用于考虑纵向振动的二阶梯度材料。基于数值求解的热力学一致模型,可以证明基于自适应滤波的系统识别可以有效地用于二阶梯度材料领域的窄带和宽带信号。研究还发现,通过识别简单材料和梯度材料的差异,可以对材料行为进行状态监测和梯度效应检测。
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引用次数: 0
Dynamics and Stability of Double-Walled Carbon Nanotube Cantilevers Conveying Fluid in an Elastic Medium 在弹性介质中输送流体的双壁碳纳米管悬臂的动力学和稳定性
Pub Date : 2024-03-27 DOI: 10.3390/dynamics4020013
V. Vassilev, G. Valchev
The paper concerns the dynamics and stability of double-walled carbon nanotubes conveying fluid. The equations of motion adopted in the current study to describe the dynamics of such nano-pipes stem from the classical Bernoulli–Euler beam theory. Several additional terms are included in the basic equations in order to take into account the influence of the conveyed fluid, the impact of the surrounding medium and the effect of the van der Waals interaction between the inner and outer single-walled carbon nanotubes constituting a double-walled one. In the present work, the flow-induced vibrations of the considered nano-pipes are studied for different values of the length of the pipe, its inner radius, the characteristics of the ambient medium and the velocity of the fluid flow, which is assumed to be constant. The critical fluid flow velocities are obtained at which such a cantilevered double-walled carbon nanotube embedded in an elastic medium loses stability.
本文涉及输送流体的双壁碳纳米管的动力学和稳定性。本研究中用于描述此类纳米管动力学的运动方程源自经典的伯努利-欧勒梁理论。为了考虑输送流体的影响、周围介质的影响以及构成双壁碳纳米管的内外单壁碳纳米管之间范德华相互作用的影响,在基本方程中加入了几个附加项。在本研究中,针对管道长度、内半径、周围介质特性和假定为恒定的流体流速的不同值,研究了所考虑的纳米管道的流动诱导振动。在临界流体流速下,嵌入弹性介质中的悬臂双壁碳纳米管将失去稳定性。
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引用次数: 0
Exploiting Domain Partition in Response Function-Based Dynamic Surrogate Modeling: A Continuous Crystallizer Study 在基于响应函数的动态代理建模中利用领域划分:连续结晶器研究
Pub Date : 2024-03-26 DOI: 10.3390/dynamics4020012
A. Di Pretoro, L. Montastruc, Stéphane Negny
Given the exponential rise in the amount of data requiring processing in all engineering fields, phenomenological models have become computationally cumbersome. For this reason, more efficient data-driven models have been recently used with the purpose of substantially reducing simulation computational times. However, especially in process engineering, the majority of the proposed surrogate models address steady-state problems, while poor studies refer to dynamic simulation modeling. For this reason, using a response function-based approach, a crystallization unit case study was set up in order to derive a dynamic data-driven model for crystal growth whose characteristic differential parameters are derived via Response Surface Methodology. In particular, multiple independent variables were considered, and a well-established sampling technique was exploited for sample generation. Then, different sample sizes were tested and compared in terms of accuracy indicators. Finally, the domain partition strategy was exploited in order to show its relevant impact on the final model accuracy. In conclusion, the outcome of this study proved that the proposed procedure is a suitable methodology for dynamic system metamodeling, as it shows good compliance and relevant improvement in terms of computational time. In terms of future research perspectives, testing the proposed procedure on different systems and in other research fields would allow for greater improvement and would, eventually, extend its validity.
鉴于所有工程领域需要处理的数据量呈指数级增长,现象学模型已变得计算繁琐。因此,最近开始使用更高效的数据驱动模型,以大幅缩短模拟计算时间。然而,特别是在过程工程领域,大多数提出的代用模型都是针对稳态问题的,而针对动态模拟建模的研究却很少。为此,我们采用基于响应函数的方法,建立了一个结晶单元案例研究,以推导出晶体生长的动态数据驱动模型,其特征微分参数是通过响应面方法得出的。其中,考虑了多个自变量,并利用成熟的抽样技术生成样本。然后,测试了不同的样本大小,并就精度指标进行了比较。最后,还利用了领域划分策略,以显示其对最终模型准确性的相关影响。总之,这项研究的结果证明,所提出的程序是一种适用于动态系统元建模的方法,因为它在计算时间方面显示出良好的合规性和相关的改进。就未来的研究前景而言,在不同系统和其他研究领域对所提出的程序进行测试,将使其得到更大的改进,并最终扩大其有效性。
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引用次数: 0
Iterated Crank–Nicolson Method for Peridynamic Models 用于周向动力学模型的迭代曲柄-尼科尔森法
Pub Date : 2024-03-15 DOI: 10.3390/dynamics4010011
Jinjie Liu, Samuel Appiah-Adjei, M. Brio
In this paper, we explore the iterated Crank–Nicolson (ICN) algorithm for the one-dimensional peridynamic model. The peridynamic equation of motion is an integro-differential equation that governs structural deformations such as fractures. The ICN method was originally developed for hyperbolic advection equations. In peridynamics, we apply the ICN algorithm for temporal discretization and the midpoint quadrature method for spatial integration. Several numerical tests are carried out to evaluate the performance of the ICN method. In general, the ICN method demonstrates second-order accuracy, consistent with the Störmer–Verlet (SV) method. When the weight is 1/3, the ICN method behaves as a third-order Runge–Kutta method and maintains strong stability-preserving (SSP) properties for linear problems. Regarding energy conservation, the ICN algorithm maintains at least second-order accuracy, making it superior to the SV method, which converges linearly. Furthermore, selecting a weight of 0.25 results in fourth-order superconvergent energy variation for the ICN method. In this case, the ICN method exhibits energy variation similar to that of the fourth-order Runge–Kutta method but operates approximately 20% faster. Higher-order convergence for energy can also be achieved by increasing the number of iterations in the ICN method.
在本文中,我们探讨了一维周向动力学模型的迭代 Crank-Nicolson 算法(ICN)。围动力学运动方程是一个控制断裂等结构变形的积分微分方程。ICN 方法最初是针对双曲平流方程开发的。在周动力学中,我们采用 ICN 算法进行时间离散化,并采用中点正交法进行空间积分。为了评估 ICN 方法的性能,我们进行了几次数值测试。总体而言,ICN 方法与 Störmer-Verlet (SV) 方法一致,表现出二阶精度。当权重为 1/3 时,ICN 方法表现为三阶 Runge-Kutta 方法,并对线性问题保持较强的稳定性(SSP)。在能量守恒方面,ICN 算法至少保持了二阶精度,这使其优于线性收敛的 SV 方法。此外,选择 0.25 的权重会使 ICN 方法产生四阶超收敛能量变化。在这种情况下,ICN 方法的能量变化与四阶 Runge-Kutta 方法相似,但运行速度快了约 20%。通过增加 ICN 方法的迭代次数,也可以实现能量的高阶收敛。
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引用次数: 0
Phase Diagram of Nuclear Pastas in Neutron Star Crusts 中子星外壳中的核糊状物相图
Pub Date : 2024-02-22 DOI: 10.3390/dynamics4010009
Jorge A. Muñoz, Jorge A. López
Two neural networks were trained to predict, respectively, the Euler characteristic and the curvature of nuclear pastas in neutron star crust conditions generated by molecular dynamics simulations of neutron star matter with 0.1 < x < 0.5, 0.040 fm−3 < ρ < 0.085 fm−3 (0.68 × 1014 g/cm3 < ρ < 1.43 × 1014 g/cm3), and 0.2 MeV < T < 4.0 MeV, where x is proton content, the density is ρ, and the temperature is T. The predictions of the two networks were combined to determine the nuclear pasta phase that is thermodynamically stable at a given x, ρ, and T, and a three-dimensional phase diagram that extrapolated slightly the regions of existing molecular dynamics data was computed. The jungle gym and anti-jungle gym structures are prevalent at high temperature and low density, while the anti-jungle gym and anti-gnocchi structures dominate at high temperature and high density. A diversity of structures exist at low temperatures and intermediate density and proton content. The trained models used in this work are open access and available at a public repository to promote comparison to pastas obtained with other models.
对两个神经网络进行了训练,以分别预测中子星地壳条件下核面食的欧拉特性和曲率,中子星物质的分子动力学模拟产生了0.1 < x < 0.5、0.040 fm-3 < ρ < 0.085 fm-3 (0.68 × 1014 g/cm3 < ρ < 1.43 × 1014 g/cm3)和0.2 MeV < T < 4.结合两个网络的预测结果,确定了在给定的 x、ρ 和 T 条件下热力学稳定的核面相,并计算了根据现有分子动力学数据区域推断的三维相图。丛林健身房和反丛林健身房结构在高温和低密度条件下普遍存在,而反丛林健身房和反格诺基结构则在高温和高密度条件下占主导地位。在低温、中等密度和质子含量条件下,存在多种结构。这项工作中使用的训练有素的模型是开放式的,可在公共资料库中查阅,以便与使用其他模型获得的面食进行比较。
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引用次数: 0
Development and Validation of a Compressible Reacting Gas-Dynamic Flow Solver for Supersonic Combustion 开发和验证用于超音速燃烧的可压缩反应气体动力流求解器
Pub Date : 2024-02-11 DOI: 10.3390/dynamics4010008
Anvar Gilmanov, P. Gokulakrishnan, M. Klassen
An approach based on the OpenFOAM library has been developed to solve a high-speed, multicomponent mixture of a reacting, compressible flow. This work presents comprehensive validation of the newly developed solver, called compressibleCentralReactingFoam, with different supersonic flows, including shocks, expansion waves, and turbulence–combustion interaction. The comparisons of the simulation results with experimental and computational data confirm the fidelity of this solver for problems involving multicomponent high-speed reactive flows. The gas dynamics of turbulence–chemistry interaction are modeled using a partially stirred reactor formulation and provide promising results to better understand the complex physics involved in supersonic combustors. A time-scale analysis based on local Damköhler numbers reveals different regimes of turbulent combustion. In the core of the jet flow, the Damköhler number is relatively high, indicating that the reaction time scale is smaller than the turbulent mixing time scale. This means that the combustion is controlled by turbulent mixing. In the shear layer, where the heat release rate and the scalar dissipation rate have the highest value, the flame is stabilized due to finite rate chemistry with small Damköhler numbers and a limited fraction of fine structure. This solver allows three-dimensional gas dynamic simulation of high-speed multicomponent reactive flows relevant to practical combustion applications.
我们开发了一种基于 OpenFOAM 库的方法,用于求解可压缩反应流的高速多组分混合物。这项工作对新开发的求解器(名为 compressibleCentralReactingFoam)进行了全面验证,该求解器可用于不同的超音速流动,包括冲击、膨胀波和湍流与燃烧的相互作用。模拟结果与实验和计算数据的比较证实了该求解器对于涉及多组分高速反应流问题的保真度。湍流-化学相互作用的气体动力学模型采用了部分搅拌反应器公式,并为更好地理解超音速燃烧器中涉及的复杂物理现象提供了有希望的结果。基于局部达姆克勒数的时间尺度分析揭示了湍流燃烧的不同状态。在喷射流的核心部分,达姆克勒数相对较高,表明反应时间尺度小于湍流混合时间尺度。这意味着燃烧受湍流混合控制。在热释放速率和标量耗散速率值最高的剪切层中,由于达姆克勒数较小和细小结构部分有限,有限速率化学反应使火焰趋于稳定。这种求解器可以对与实际燃烧应用相关的高速多组分反应流进行三维气体动力学模拟。
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引用次数: 0
Development and Validation of a Compressible Reacting Gas-Dynamic Flow Solver for Supersonic Combustion 开发和验证用于超音速燃烧的可压缩反应气体动力流求解器
Pub Date : 2024-02-11 DOI: 10.3390/dynamics4010008
Anvar Gilmanov, P. Gokulakrishnan, M. Klassen
An approach based on the OpenFOAM library has been developed to solve a high-speed, multicomponent mixture of a reacting, compressible flow. This work presents comprehensive validation of the newly developed solver, called compressibleCentralReactingFoam, with different supersonic flows, including shocks, expansion waves, and turbulence–combustion interaction. The comparisons of the simulation results with experimental and computational data confirm the fidelity of this solver for problems involving multicomponent high-speed reactive flows. The gas dynamics of turbulence–chemistry interaction are modeled using a partially stirred reactor formulation and provide promising results to better understand the complex physics involved in supersonic combustors. A time-scale analysis based on local Damköhler numbers reveals different regimes of turbulent combustion. In the core of the jet flow, the Damköhler number is relatively high, indicating that the reaction time scale is smaller than the turbulent mixing time scale. This means that the combustion is controlled by turbulent mixing. In the shear layer, where the heat release rate and the scalar dissipation rate have the highest value, the flame is stabilized due to finite rate chemistry with small Damköhler numbers and a limited fraction of fine structure. This solver allows three-dimensional gas dynamic simulation of high-speed multicomponent reactive flows relevant to practical combustion applications.
我们开发了一种基于 OpenFOAM 库的方法,用于求解可压缩反应流的高速多组分混合物。这项工作对新开发的求解器(名为 compressibleCentralReactingFoam)进行了全面验证,该求解器可用于不同的超音速流动,包括冲击、膨胀波和湍流与燃烧的相互作用。模拟结果与实验和计算数据的比较证实了该求解器对于涉及多组分高速反应流问题的保真度。湍流-化学相互作用的气体动力学模型采用了部分搅拌反应器公式,并为更好地理解超音速燃烧器中涉及的复杂物理现象提供了有希望的结果。基于局部达姆克勒数的时间尺度分析揭示了湍流燃烧的不同状态。在喷射流的核心部分,达姆克勒数相对较高,表明反应时间尺度小于湍流混合时间尺度。这意味着燃烧受湍流混合控制。在热释放速率和标量耗散速率值最高的剪切层中,由于达姆克勒数较小和细小结构部分有限,有限速率化学反应使火焰趋于稳定。这种求解器可以对与实际燃烧应用相关的高速多组分反应流进行三维气体动力学模拟。
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引用次数: 0
Analysis of Wind Turbine Wake Dynamics by a Gaussian-Core Vortex Lattice Technique 利用高斯核心涡流晶格技术分析风力涡轮机的风浪动力学特性
Pub Date : 2024-02-01 DOI: 10.3390/dynamics4010006
Apurva Baruah, Fernando Ponta
The development and deployment of the next generation of wind energy systems calls for simulation tools that model the entire wind farm while balancing accuracy and computational cost. A full-system wind farm simulation must consider the atmospheric inflow, the wakes and consequent response of the multiple turbines, and the implementation of the appropriate farm-collective control strategies that optimize the entire wind farm’s output. In this article, we present a novel vortex lattice model that enables the effective representation of the complex vortex wake dynamics of the turbines in a farm subject to transient inflow conditions. This work extends the capabilities of our multi-physics suite, CODEF, to include the capability to simulate the wakes and the high-fidelity aeroelastic response of multiple turbines in a wind farm. Herein, we compare the results of our GVLM technique with the LiDAR measurements obtained at Sandia National Laboratories’ SWiFT facility. The comparison shows remarkable similarities between the simulation and field measurements of the wake velocity. These similarities demonstrate our model’s capabilities in capturing the entire wake of a wind turbine at a significantly reduced computational cost as compared to other techniques.
下一代风能系统的开发和部署需要既能模拟整个风电场,又能兼顾精度和计算成本的模拟工具。全系统风电场仿真必须考虑大气流入、多个涡轮机的摆动和随之而来的响应,以及实施适当的风电场集合控制策略,以优化整个风电场的输出。在这篇文章中,我们介绍了一种新型涡流网格模型,该模型可有效表示风电场中涡轮机在瞬态流入条件下的复杂涡流尾流动态。这项工作扩展了我们的多物理场套件 CODEF 的功能,使其能够模拟风电场中多个涡轮机的涡流和高保真气动弹性响应。在此,我们将 GVLM 技术的结果与桑迪亚国家实验室 SWiFT 设施获得的激光雷达测量结果进行了比较。比较结果表明,模拟结果与现场测量的尾流速度非常相似。这些相似性表明,与其他技术相比,我们的模型能够捕捉风力涡轮机的整个尾流,而且计算成本大大降低。
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引用次数: 0
Analysis of Wind Turbine Wake Dynamics by a Gaussian-Core Vortex Lattice Technique 利用高斯核心涡流晶格技术分析风力涡轮机的风浪动力学特性
Pub Date : 2024-02-01 DOI: 10.3390/dynamics4010006
Apurva Baruah, Fernando Ponta
The development and deployment of the next generation of wind energy systems calls for simulation tools that model the entire wind farm while balancing accuracy and computational cost. A full-system wind farm simulation must consider the atmospheric inflow, the wakes and consequent response of the multiple turbines, and the implementation of the appropriate farm-collective control strategies that optimize the entire wind farm’s output. In this article, we present a novel vortex lattice model that enables the effective representation of the complex vortex wake dynamics of the turbines in a farm subject to transient inflow conditions. This work extends the capabilities of our multi-physics suite, CODEF, to include the capability to simulate the wakes and the high-fidelity aeroelastic response of multiple turbines in a wind farm. Herein, we compare the results of our GVLM technique with the LiDAR measurements obtained at Sandia National Laboratories’ SWiFT facility. The comparison shows remarkable similarities between the simulation and field measurements of the wake velocity. These similarities demonstrate our model’s capabilities in capturing the entire wake of a wind turbine at a significantly reduced computational cost as compared to other techniques.
下一代风能系统的开发和部署需要既能模拟整个风电场,又能兼顾精度和计算成本的模拟工具。全系统风电场仿真必须考虑大气流入、多个涡轮机的摆动和随之而来的响应,以及实施适当的风电场集合控制策略,以优化整个风电场的输出。在这篇文章中,我们介绍了一种新型涡流网格模型,该模型可有效表示风电场中涡轮机在瞬态流入条件下的复杂涡流尾流动态。这项工作扩展了我们的多物理场套件 CODEF 的功能,使其能够模拟风电场中多个涡轮机的涡流和高保真气动弹性响应。在此,我们将 GVLM 技术的结果与桑迪亚国家实验室 SWiFT 设施获得的激光雷达测量结果进行了比较。比较结果表明,模拟结果与现场测量的尾流速度非常相似。这些相似性表明,与其他技术相比,我们的模型能够捕捉风力涡轮机的整个尾流,而且计算成本大大降低。
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引用次数: 0
New Types of Derivative Non-linear Schrödinger Equations Related to Kac–Moody Algebra A2(1) 与 Kac-Moody 代数 A2(1) 有关的新型衍生非线性薛定谔方程
Pub Date : 2024-01-18 DOI: 10.3390/dynamics4010005
A. A. Stefanov
We derive a new system of integrable derivative non-linear Schrödinger equations with an L operator, quadratic in the spectral parameter with coefficients belonging to the Kac–Moody algebra A2(1). The construction of the fundamental analytic solutions of L is outlined and they are used to introduce the scattering data, thus formulating the scattering problem for the Lax pair L,M.
我们导出了一个新的可积分导数非线性薛定谔方程系统,该系统包含一个 L 算子,其系数属于 Kac-Moody 代数 A2(1)的谱参数二次方。概述了 L 基本解析解的构造,并用它们引入散射数据,从而提出了 Lax 对 L,M 的散射问题。
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引用次数: 0
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Dynamics
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