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Any order spectral volume methods for diffusion equations using the local discontinuous Galerkin formulation 用局部不连续伽辽金公式求解扩散方程的任意阶谱体积法
IF 1.9 3区 数学 Q2 Mathematics Pub Date : 2023-01-06 DOI: 10.1051/m2an/2023003
Jing An, Waixiang Cao
In this paper, we present and study two spectral volume (SV) schemes of arbitrary order for diffusion equations by using the local discontinuous Galerkin formulation to discretize the viscous flux. The basic idea of the scheme is to rewrite the diffusion equation into an equivalent first-order system first, and then use the SV method to solve the system. The SV scheme is designed with control volumes constructed by using the Gauss points or Radau points in subintervals of the underlying meshes, which leads to two SV schemes referred to as LSV and RSV schemes, respectively. The stability analysis for the linear diffusion equations based on alternating fluxes are provided, and optimal error estimates are established for both the exact solution and the auxiliary variable. Furthermore, a rigorous mathematical proof are given to demonstrate that the proposed RSV method is identical to the standard LDG method when applied to constant diffusion problems. Numerical experiments are presented to demonstrate the stability, accuracy and performance of the two SV schemes for both linear and nonlinear diffusion equations.
本文提出并研究了两种任意阶的扩散方程谱体积格式,利用局部不连续伽辽金公式对粘性通量进行离散化。该方案的基本思想是先将扩散方程改写为等效的一阶系统,然后用SV法求解该系统。SV方案的控制体积是利用底层网格的子区间中的Gauss点或Radau点构建的,这就产生了两种SV方案,分别称为LSV和RSV方案。对基于交变通量的线性扩散方程进行了稳定性分析,建立了精确解和辅助变量的最优误差估计。此外,通过严密的数学证明,表明RSV方法在常扩散问题上与标准LDG方法是一致的。数值实验验证了这两种格式对线性和非线性扩散方程的稳定性、精度和性能。
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引用次数: 1
Exponential stabilization for carbon nanotubes modeled as Timoshenko beams with thermoelastic effects 具有热弹性效应的Timoshenko光束型碳纳米管的指数稳定性
IF 1.9 3区 数学 Q2 Mathematics Pub Date : 2023-01-04 DOI: 10.1051/m2an/2023002
Anderson de Jesus Araújo Ramos, M. Rincon, Rodrigo L. R. Madureira, M. Freitas
In this article we consider the problem of heat conduction in carbon nanotubes modeled like Timoshenko beams, inspired by the work of J. Yoon textit{et al.} (Composites Part B: Engineering, textbf{35}(2), 87--93. 2004). Using the theory of semigroups of linear operators, we prove the well-posedness of the problem and the exponential stabilization of the total energy of the system of differential equations, partially damped, without assuming the known relationship of equality of wave velocities. Furthermore, we analyze the fully discrete problem using a finite difference scheme, introduced by a spatiotemporal discretization that combines explicit and implicit integration methods. We show the construction of numerical energy and simulations that prove our theoretical exponential decay results and display the convergence rates.
在这篇文章中,我们考虑了像Timoshenko光束一样的碳纳米管的热传导问题,灵感来自J. Yoontextit{等人}的工作(复合材料B部分:工程,textbf{35}(2),87—93)。2004)。利用线性算子的半群理论,在不假设已知波速相等关系的情况下,证明了问题的适定性和部分阻尼微分方程组总能量的指数镇定性。此外,我们使用有限差分格式分析完全离散问题,该格式由结合显式和隐式积分方法的时空离散化引入。我们展示了数值能量的构造和模拟,证明了我们的理论指数衰减结果并显示了收敛速度。
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引用次数: 1
Analysis of a method to compute mixed-mode stress intensity factors for non-planar cracks in three-dimensions 三维非平面裂纹混合模态应力强度因子计算方法分析
IF 1.9 3区 数学 Q2 Mathematics Pub Date : 2023-01-03 DOI: 10.1051/m2an/2023001
Benjamin E. Grossman‐Ponemon, M. Negri, A. Lew
In this work, we present and prove results underlying a method which uses functionals derived from the interaction integral to approximate the stress intensity factors along a three-dimensional crack front. We first prove that the functionals possess a pair of important properties. The functionals are well-defined and continuous for square-integrable tensor fields, such as the gradient of a finite element solution. Furthermore, the stress intensity factors are representatives of such functionals in a space of functions over the crack front. Our second result is an error estimate for the numerical stress intensity factors computed via our method. The latter property of the functionals provides a recipe for numerical stress intensity factors; we apply the functionals to the gradient of a finite element approximation for a specific set of crack front variations, and we calculate the stress intensity factors by inverting the mass matrix for those variations.
在这项工作中,我们提出并证明了一种方法的结果,该方法使用从相互作用积分中导出的泛函来近似三维裂缝前缘的应力强度因子。我们首先证明泛函具有一对重要的性质。对于平方可积张量场,如有限元解的梯度,泛函是定义良好且连续的。此外,应力强度因子是这些泛函在裂缝前缘的函数空间中的代表。我们的第二个结果是通过我们的方法计算的数值应力强度因子的误差估计。泛函的后一种性质为计算应力强度因子提供了一种方法;我们将函数应用于一组特定裂纹前缘变化的有限元近似梯度,并通过对这些变化的质量矩阵进行反求来计算应力强度因子。
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引用次数: 0
Implicit discretization of Lagrangian gas dynamics 拉格朗日气体动力学的隐式离散化
IF 1.9 3区 数学 Q2 Mathematics Pub Date : 2022-12-20 DOI: 10.1051/m2an/2022102
Alexiane Plessier, S. Del Pino, B. Després
We construct an original framework based on convex analysis to prove the existence and uniqueness of a solution to a class of implicit numerical schemes. We propose an application of this general framework in the case of a new non linear implicit scheme for the 1D Lagrangian gas dynamics equations. We provide numerical illustrations that corroborate our proof of unconditional stability for this non linear implicit scheme.
为了证明一类隐式数值格式解的存在唯一性,我们构造了一个基于凸分析的原始框架。我们在一维拉格朗日气体动力学方程的一种新的非线性隐式格式中提出了这种一般框架的应用。我们给出了数值例证来证实我们对这种非线性隐式格式的无条件稳定性的证明。
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引用次数: 0
Singular versus boundary arcs for aircraft trajectory optimization in climbing phase 爬升阶段飞机轨迹优化的奇异弧与边界弧
IF 1.9 3区 数学 Q2 Mathematics Pub Date : 2022-12-13 DOI: 10.1051/m2an/2022101
O. Cots, J. Gergaud, D. Goubinat, B. Wembe
In this article, we are interested in optimal aircraft trajectories in climbing phase. We consider the cost index criterion which is a convex combination of the time-to-climb and the fuel consumption. We assume that the thrust is constant and we control the air slope of the aircraft. This optimization problem is modeled as a Mayer optimal control problem with a single-input affine dynamics in the control and with two pure state constraints, limiting the Calibrated AirSpeed (CAS) and the Mach speed. The candidates as minimizers are selected among a set of extremals given by the maximum principle. We first analyze the minimum time-to-climb problem with respect to the bounds of the state constraints, combining small time analysis, indirect multiple shooting and homotopy methods with monitoring. This investigation emphasizes two strategies: the common CAS/Mach procedure in aeronautics and the classical Bang-Singular-Bang policy in control theory. We then compare these two procedures for the cost index criterion.
在本文中,我们感兴趣的是飞机爬升阶段的最优轨迹。考虑了爬升时间和燃油消耗的凸组合成本指标准则。我们假设推力是恒定的,我们控制飞机的气流斜率。该优化问题被建模为一个Mayer最优控制问题,在控制中具有单输入仿射动力学,并具有两个纯状态约束,限制了校准空速(CAS)和马赫速度。作为最小值的候选者是从由极大值原理给出的一组极值中选出的。我们首先结合小时间分析、间接多次射击和同伦方法与监测相结合,根据状态约束的边界分析了最小爬升时间问题。本文着重研究了两种策略:航空学中常用的CAS/Mach程序和控制理论中经典的bang - singularity - bang策略。然后,我们比较这两种程序的成本指数标准。
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引用次数: 1
Superconvergence and postprocessing of the continuous Galerkin method for nonlinear Volterra integro-differential equations 非线性Volterra积分微分方程的连续Galerkin法的超收敛性和后处理
IF 1.9 3区 数学 Q2 Mathematics Pub Date : 2022-12-08 DOI: 10.1051/m2an/2022100
Mingzhu Zhang, X. Mao, Lijun Yi
We propose a novel postprocessing technique for improving the global accuracy of the continuous Galerkin (CG) method for nonlinear Volterra integro-differential equations. The key idea behind the postprocessing technique is to add a higher order Lobatto polynomial of degree k + 1 to the CG approximation of degree k . We first show that the CG method superconverges at the nodal points of the time partition. We further prove that the postprocessed CG approximation converges one order faster than the unprocessed CG approximation in the L 2 -, H 1 - and L ∞ -norms. As a by-product of the postprocessed superconvergence results, we construct several a posteriori error estimators and prove that they are asymptotically exact. Numerical examples are presented to highlight the superconvergence properties of the postprocessed CG approximations and the robustness of the a posteriori error estimators.
为了提高非线性Volterra积分-微分方程连续伽辽金(CG)方法的全局精度,提出了一种新的后处理技术。后处理技术背后的关键思想是将k + 1次的高阶Lobatto多项式添加到k次的CG近似中。我们首先证明了CG方法在时间分区的节点处是超收敛的。进一步证明了在l2 -、h1 -和L∞-范数下,后处理的CG近似比未处理的CG近似收敛快一个阶。作为后处理超收敛结果的副产品,我们构造了几个后验误差估计量,并证明了它们是渐近精确的。通过数值算例说明了后处理CG逼近的超收敛性和后验误差估计的鲁棒性。
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引用次数: 2
Erratum to: "Sparse-grid polynomial interpolation approximation and integration for parametric and stochastic elliptic PDEs with lognormal inputs" [ESAIM: M2AN 55(2021) 1163--1198] “具有对数正态输入的参数和随机椭圆偏微分方程的稀疏网格多项式插值逼近和积分”的勘误[ESAIM: M2AN 55(2021) 1163—1198]
IF 1.9 3区 数学 Q2 Mathematics Pub Date : 2022-11-29 DOI: 10.1051/m2an/2022097
D. Đinh
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引用次数: 1
An EMA-conserving, pressure-robust and Re-semi-robust reconstruction method for incompressible Navier-Stokes simulations 不可压缩Navier-Stokes模拟的一种ema守恒、压力鲁棒和re-半鲁棒重建方法
IF 1.9 3区 数学 Q2 Mathematics Pub Date : 2022-11-17 DOI: 10.1051/m2an/2022093
Xu Li, H. Rui
Proper EMA-balance (balance of kinetic energy, linear momentum and angular momentum), pressure-robustness and $Re$-semi-robustness ($Re$: Reynolds number) are three important properties of Navier--Stokes simulations with exactly divergence-free elements. This EMA-balance makes a method conserve kinetic energy, linear momentum and angular momentum in an appropriate sense; pressure-robustness means that the velocity errors are independent of the pressure; $Re$-semi-robustness means that the constants appearing in the error bounds of kinetic and dissipation energies do not explicitly depend on inverse powers of the viscosity. In this paper, based on the pressure-robust reconstruction framework and certain suggested reconstruction operators in [A. Linke and C. Merdon, {it Comput. Methods Appl. Mech. Engrg.} 311 (2016), 304-326], we propose a reconstruction method for a class of non-divergence-free simplicial elements which admits almost all the above properties. The only exception is the energy balance, where kinetic energy should be replaced by a suitably redefined discrete energy. The lowest order case is the Bernardi--Raugel element on general shape-regular meshes. Some numerical comparisons with exactly divergence-free methods, the original pressure-robust reconstruction methods and the EMAC method are provided to confirm our theoretical results.
适当的ema -平衡(动能、线性动量和角动量的平衡)、压力-鲁棒性和$Re$-半鲁棒性($Re$:雷诺数)是具有完全无散度元素的Navier- Stokes模拟的三个重要性质。这种ema平衡使一种方法在适当意义上守恒了动能、线动量和角动量;压力鲁棒性是指速度误差与压力无关;Re -半鲁棒性意味着出现在动能和耗散能误差范围内的常数不明确地依赖于粘度的逆幂。本文基于[A]中的压力-鲁棒重构框架和若干建议重构算子。林克和C.默顿,{it计算机。方法:。动力机械。Engrg。{311(2016), 304-326],我们提出了一类非无散度简单元的重构方法,该方法几乎具有上述所有性质。唯一的例外是能量平衡,动能应该被适当重新定义的离散能量所取代。最低阶的情况是一般形状规则网格上的Bernardi- Raugel单元。通过与完全无发散方法、原始压力鲁棒重建方法和EMAC方法的数值比较,验证了我们的理论结果。
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引用次数: 2
Quadratic stability of flux limiters 磁通限制器的二次稳定性
IF 1.9 3区 数学 Q2 Mathematics Pub Date : 2022-11-13 DOI: 10.1051/m2an/2022092
B. Després
We propose a novel approach to study the quadratic stability of 2D flux limiters for non expansive transport equations. The theory is developed for the constant coefficient case on a cartesian grid. The convergence of the fully discrete nonlinear scheme is established in 2D with a rate not less than) in quadratic norm. It is a way to bypass the Goodman-Leveque obstruction Theorem. A new nonlinear scheme with corner correction is proposed. The scheme is formally second-order accurate away from characteristics points, satisfies the maximum principle and is proved to be convergent in quadratic norm. It is tested on simple numerical problems.
我们提出了一种新的方法来研究非膨胀输运方程的二维通量限制器的二次稳定性。该理论适用于直角网格上的常系数情况。在二维条件下,以不小于2次范数的速率建立了完全离散非线性格式的收敛性。这是一种绕过Goodman-Leveque阻塞定理的方法。提出了一种新的带角点校正的非线性格式。该格式在远离特征点处具有二阶精度,满足极大值原理,并在二次范数上具有收敛性。对简单的数值问题进行了测试。
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引用次数: 1
Developing and analyzing an explicit unconditionally stable finite element scheme for an equivalent B´erenger’s PML model * 开发并分析了等效B ' erenger的PML模型的显式无条件稳定有限元格式*
IF 1.9 3区 数学 Q2 Mathematics Pub Date : 2022-10-07 DOI: 10.1051/m2an/2022086
Yunqing Huang, Jichun Li, Xin Liu
The original B´erenger’s perfectly matched layer (PML) was quite effective in simulating wave propagation problem in unbounded domains. But its stability is very challenging to prove. Later, some equivalent PML models were developed by B´ecache and Joly [4] and their stabilities were established. Hence studying and developing efficicent numerical methods for solving those equivalent PML models are needed and interesting. Here we propose a novel explicit unconditionally stable finite element scheme to solve an equivalent B´erenger’s PML model. Both the stability and convergence analysis are proved for the proposed scheme. Numerical results justifying the theoretical analysis are presented. We also demonstrate the effectiveness of this PML in simulating wave propagation in the free space. To our best knowledge, this is the first explicit unconditionally stable finite element scheme developed for this PML model.
原始的B´erenger完美匹配层(PML)可以很好地模拟无界域中的波传播问题。但它的稳定性很难证明。后来,B´ecache和Joly[4]开发了一些等效的PML模型,并建立了它们的稳定性。因此,研究和开发求解这些等效PML模型的有效数值方法是非常必要和有趣的。本文提出了一种新的显式无条件稳定有限元格式来求解等效B´erenger的PML模型。证明了该方案的稳定性和收敛性。给出了验证理论分析的数值结果。我们还证明了该PML在模拟自由空间中的波传播方面的有效性。据我们所知,这是针对该PML模型开发的第一个明确的无条件稳定有限元方案。
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引用次数: 1
期刊
Esaim-Mathematical Modelling and Numerical Analysis-Modelisation Mathematique et Analyse Numerique
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