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Two-dimensional equilibrium configurations in Korteweg fluids Korteweg流体的二维平衡构型
IF 0.7 Q3 Engineering Pub Date : 2022-01-01 DOI: 10.2298/tam220930008g
M. Gorgone, F. Oliveri, A. Ricciardello, P. Rogolino
In this paper, after reviewing the form of the constitutive equations for a third grade Korteweg fluid, recently derived by means of an extended Liu procedure, an equilibrium problem is investigated. By considering a two-dimensional setting, a single nonlinear elliptic equation is derived such that the equilibrium conditions are identically satisfied. Such an equation is discussed both analytically and numerically. Moreover, by considering a particular boundary value problem of Dirichlet type, some preliminary numerical solutions are presented.
本文在回顾了最近用扩展Liu方法导出的三阶Korteweg流体的本构方程的形式之后,研究了平衡问题。考虑二维环境,导出了满足平衡条件的单一非线性椭圆方程。对这种方程进行了解析和数值讨论。此外,考虑一类特殊的Dirichlet型边值问题,给出了一些初步的数值解。
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引用次数: 0
Tulczyjew’s triplet for lie groups III: Higher order dynamics and reductions for iterated bundles 李群的Tulczyjew三重态III:迭代束的高阶动力学和约简
IF 0.7 Q3 Engineering Pub Date : 2021-02-22 DOI: 10.2298/TAM210312009E
Ougul Esen, H. Gumral, S. Sutlu
Given a Lie group G, we elaborate the dynamics on T+T+G and T+TG, which is given by a Hamiltonian, as well as the dynamics on the Tulczyjew symplectic space TT+G, which may be defined by a Lagrangian or a Hamiltonian function. As the trivializations we adapted respect the group structures of the iterated bundles, we exploit all possible subgroup reductions (Poisson, symplectic or both) of higher order dynamics.
在给定李群G的情况下,给出了由哈密顿函数给出的T+T+G和T+TG上的动力学,以及由拉格朗日函数或哈密顿函数定义的图尔奇犹太辛空间TT+G上的动力学。由于我们所采用的琐屑化方法尊重迭代束的群结构,我们利用了所有可能的高阶动力学的子群约简(泊松,辛或两者)。
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引用次数: 4
A time-dependent metric graph with a fourth-order operator on the edges 边上有四阶算子的时变度量图
IF 0.7 Q3 Engineering Pub Date : 2021-01-01 DOI: 10.2298/tam200928007b
I. Blinova, A.S. Gnedash, I. Popov
The metric graph model is suggested for description of elastic vibration in a network of rods under the assumption that the rod lengths vary in time. A single rod and star-like graph are considered. Influence of the length variation law on the vibration distribution is investigated. For high-frequency length variation one observes a fast transition to high-frequency amplitude distribution
在假设杆长随时间变化的情况下,提出了描述杆网弹性振动的度量图模型。考虑一个单杆和星形图。研究了长度变化规律对振动分布的影响。对于高频长度变化,可以观察到向高频振幅分布的快速过渡
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引用次数: 0
Classical solutions for a class of nonlinear wave equations 一类非线性波动方程的经典解
IF 0.7 Q3 Engineering Pub Date : 2021-01-01 DOI: 10.2298/tam201123013g
S. Georgiev, K. Mebarki, K. Zennir
We study a class of initial value problems subject to nonlinear partial differential equations of hyperbolic type. A new topological approach is applied to prove the existence of nontrivial nonnegative solutions. More precisely, we propose a new integral representation of the solutions for the considered initial value problems and using this integral representation we establish existence of classical solutions for the considered classes of nonlinear wave equations.
研究了一类双曲型非线性偏微分方程的初值问题。应用一种新的拓扑方法来证明非平凡非负解的存在性。更准确地说,我们提出了所考虑的初值问题解的一种新的积分表示,并利用这种积分表示建立了所考虑的一类非线性波动方程经典解的存在性。
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引用次数: 0
Stability of pinned-rotationally restrained arches 旋压约束拱的稳定性
IF 0.7 Q3 Engineering Pub Date : 2021-01-01 DOI: 10.2298/tam200402010k
L. Peter
The article aims to find the buckling loads for pinned?rotationally restrained shallow circular arches in terms of the rotational end stiffness, geometry and material distribution. The loading is a concentrated vertical force placed at the crown. A geometrically nonlinear model is presented which relates not only the axial force but also the bending moment to the membrane strain. The nonlinear load-strain relationship is established between the strain and load parameters. This equation is then solved and evaluated analytically. It turns out that the stiffness of the end-restraint has, in general, a significant effect on the lowest buckling load. At the same time, some geometries are not affected by this. As the stiffness becomes zero, the arch is pinned-pinned and as the stiffness tends to infinity, the arch behaves as if it were pinned-fixed and has the best load-bearing abilities.
本文的目的是求出固定梁的屈曲载荷。旋转约束浅圆拱的转动端刚度,几何形状和材料分布。载荷是一个集中的垂直力放置在顶部。提出了膜应变与轴向力和弯矩之间的几何非线性模型。建立了应变与载荷参数之间的非线性载荷-应变关系。然后对这个方程进行求解和解析评估。结果表明,端部约束刚度一般对最低屈曲载荷有显著影响。同时,有些几何形状不受此影响。当刚度趋近于零时,拱处于钉钉状态;当刚度趋近于无穷大时,拱表现为钉钉固定状态,具有最佳的承载能力。
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引用次数: 1
Existence and stability results of a nonlinear Timoshenko equation with damping and source terms 具有阻尼和源项的非线性Timoshenko方程的存在性和稳定性结果
IF 0.7 Q3 Engineering Pub Date : 2021-01-01 DOI: 10.2298/TAM200703002O
Amar Ouaoua, A. Khaldi, M. Maouni
In this paper, we consider a nonlinear Timoshenko equation. First, we prove the local existence solution by the Faedo?Galerkin method, and, under suitable assumptions with positive initial energy, we prove that the local existence is global in time. Finally, the stability result is established based on Komornik?s integral inequality.
本文考虑一类非线性Timoshenko方程。首先,我们用费多?在适当的初始能量为正的假设下,证明了局部存在在时间上是全局的。最后,基于Komornik?S积分不等式。
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引用次数: 2
Noether’s theorem for Herglotz type variational problems utilizing complex fractional derivatives 利用复分数阶导数求解Herglotz型变分问题的Noether定理
IF 0.7 Q3 Engineering Pub Date : 2021-01-01 DOI: 10.2298/tam210913011j
M. Janev, T. Atanacković, S. Pilipovic
This is a review article which elaborates the results presented in [1], where the variational principle of Herglotz type with a Lagrangian that depends on fractional derivatives of both real and complex orders is formulated and the invariance of this principle under the action of a local group of symmetries is determined. The conservation law for the corresponding fractional Euler Lagrange equation is obtained and a sequence of approximations of a fractional Euler-Lagrange equation by systems of integer order equations established and analyzed.
这是一篇对文献[1]的结果进行阐述的综述文章,文中给出了依赖于实阶和复阶分数阶导数的拉格朗日的Herglotz型变分原理,并确定了该原理在局部对称群作用下的不变性。得到了相应分数阶欧拉-拉格朗日方程的守恒律,建立并分析了分数阶欧拉-拉格朗日方程的整数阶方程组的一系列近似。
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引用次数: 2
Towards viable flow simulations of small-scale rotors and blade segments 面向可行的小型转子和叶片段流动模拟
IF 0.7 Q3 Engineering Pub Date : 2021-01-01 DOI: 10.2298/tam211011008s
J. Svorcan, Aleksandar Kovačević, Dragoljub Tanović, M. Hasan
The paper focuses on the possibilities of adequately simulating complex flow fields that appear around small-scale propellers of multicopter aircraft. Such unmanned air vehicles (UAVs) are steadily gaining popularity for their diverse applications (surveillance, communication, deliveries, etc.) and the need for a viable (i.e. usable, satisfactory, practical) computational tool is also surging. From an engineering standpoint, it is important to obtain sufficiently accurate predictions of flow field variables in a reasonable amount of time so that the design process can be fast and efficient, in particular the subsequent structural and flight mechanics analyses. That is why more or less standard fluid flow models, e.g. Reynolds-averaged Navier-Stokes (RANS) equations solved by the finite volume method (FVM), are constantly being employed and validated. On the other hand, special attention must be given to various flow peculiarities occurring around the blade segments shaped like airfoils since these flows are characterized by small chords (length-scales), low speeds and, therefore, low Reynolds numbers (Re) and pronounced viscous effects. The investigated low-Re flows include both transitional and turbulent zones, laminar separation bubbles (LSBs), flow separation, as well as rotating wakes, which require somewhat specific approaches to flow modeling (advanced turbulence models, fine spatial and temporal scales, etc). Here, the conducted computations (around stationary blade segments as well as rotating rotors), closed by different turbulence models, are presented and explained. Various qualitative and quantitative results are provided, compared and discussed. The main possibilities and obstacles of each computational approach are mentioned. Where possible, numerical results are validated against experimental data. The correspondence between the two sets of results can be considered satisfactory (relative differences for the thrust coefficient amount to 15%, while they are even lower for the torque coefficient). It can be concluded that the choice of turbulence modeling (and/or resolving) greatly affects the final output, even in design operating conditions (at medium angles-of-attack where laminar, attached flow dominates). Distinctive flow phenomena still exist, and in order to be adequately simulated, a comprehensive modeling approach should be adopted.
本文的重点是充分模拟多旋翼飞机小型螺旋桨周围复杂流场的可能性。这种无人驾驶飞行器(uav)因其各种应用(监视,通信,交付等)而稳步普及,对可行(即可用,满意,实用)计算工具的需求也在激增。从工程的角度来看,在合理的时间内获得足够准确的流场变量预测是很重要的,这样设计过程才能快速有效,特别是随后的结构和飞行力学分析。这就是为什么或多或少的标准流体流动模型,例如由有限体积法(FVM)求解的reynolds -average Navier-Stokes (RANS)方程,不断被采用和验证的原因。另一方面,必须特别注意发生在翼型叶片段周围的各种流动特性,因为这些流动的特点是弦线(长度尺度)小,速度低,因此雷诺数(Re)低,并且具有明显的粘性效应。所研究的低re流包括过渡区和湍流区、层流分离泡(LSBs)、流动分离以及旋转尾迹,这需要一些特定的流动建模方法(先进的湍流模型、精细的时空尺度等)。本文给出并解释了在不同湍流模型下进行的计算(围绕静止叶片段和旋转转子)。提供、比较和讨论了各种定性和定量结果。介绍了各种计算方法的主要可能性和障碍。在可能的情况下,数值结果与实验数据进行验证。两组结果之间的对应关系可以被认为是令人满意的(推力系数的相对差异为15%,而扭矩系数的相对差异甚至更低)。可以得出结论,湍流建模(和/或解析)的选择极大地影响了最终输出,即使在设计操作条件下(在中等攻角下,层流,附流占主导地位)。独特的流动现象仍然存在,为了充分模拟,需要采用综合的建模方法。
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引用次数: 0
Micropolar fluid between two coaxial cylinders (numerical approach) 两个同轴圆柱体之间的微极流体(数值方法)
IF 0.7 Q3 Engineering Pub Date : 2021-01-01 DOI: 10.2298/tam210823012s
Duško R. Salemović, A. Dedić, B. Jovanovic
The paper describes the flow of a suspension which is a mixture of two phases: liquid and solid granules. The continuum model with microstructure is introduced, which involves two independent kinematic quantities: the velocity vector and the micro-rotation vector. The physical analogy is based on the movement of the suspension between two coaxial cylinders. The inner cylinder is stationary and the outer one rotates with constant angular velocity. This physical analogy enabled a mathematical model in a form of two coupled differential equations with variable coefficients. The aim of the paper is to present the numerical aspect of the solution for this complex mathematical model. It is assumed that the solid granules are identically oriented and that under the influence of the fluid they move translationally or rotate around the symmetry axis but the direction of their symmetry axes does not change. The solution was obtained by the ordinary finite difference method, and then the corresponding sets of points (nodes) were routed by interpolation graphics.
本文描述了一种由液体和固体颗粒两相组成的悬浮液的流动。引入了包含微观结构的连续介质模型,该模型包含两个独立的运动学量:速度矢量和微旋转矢量。物理类比是基于悬架在两个同轴气缸之间的运动。内筒是静止的,外筒以恒定的角速度旋转。这种物理上的类比使两个变系数耦合微分方程的数学模型成为可能。本文的目的是给出这个复杂数学模型的数值解。假设固体颗粒的取向相同,在流体的影响下,它们沿对称轴平移或旋转,但对称轴的方向不变。采用普通有限差分法求解,然后用插值图绘制出相应的点(节点)集。
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引用次数: 0
Use of the fractal dimension for porosity modification in aluminum foams manufactured using space holder particles 分形维数在用空间支架颗粒制造的泡沫铝孔隙度改性中的应用
IF 0.7 Q3 Engineering Pub Date : 2021-01-01 DOI: 10.2298/TAM210129005R
C. Reyes, L. Béjar, L. Pérez, C. Aguilar, C. J. Carranza, E. L. Carranza, I. Alfonso
The effect of space holder particles (SHP) fractal distribution on the porosity of aluminum foams manufactured by infiltration is studied in the present work. Physical models were used to estimate aluminum foam porosity, simulating SHP distribution for bimodal mixtures with different particle sizes and relative quantities. Results of these models were compared with mathematical models and the results obtained for experimental aluminum foams manufactured using a 332 Al-alloy base material and NaCl grains as SHP. Experimental foam structural characterization was carried out using image analysis to obtain porosity, density, wall thickness and fractal dimension, while mechanical characterization focused on the compressive Young modulus. Results show that it was possible to manufacture foams with different fractal porosities and a wide variety of unit cells, reaching a maximum of ? 68%. It was also found that pore wall thicknesses significantly decreased with the increase in the fine particles fraction. Besides, all the models presented a peak with a maximum porosity, whose values increased and shifted to low fine particles fraction with the increase in the sizes ratio. This behavior was also observed for the experimental foams with low particle size ratio. Nevertheless, for higher size ratios porosity showed an irregular behavior attributed to the mixing process.
本文研究了空间保持颗粒(SHP)分形分布对渗透法制备泡沫铝孔隙率的影响。采用物理模型估算泡沫铝孔隙率,模拟不同粒径和相对量的双峰混合物的SHP分布。将这些模型的结果与数学模型以及以332铝合金基材和NaCl晶粒为SHP制备泡沫铝的实验结果进行了比较。实验泡沫结构表征主要通过图像分析获得孔隙率、密度、壁厚和分形维数,力学表征主要集中在压缩杨氏模量上。结果表明,该方法可以制备出具有不同分形孔隙率和多种单位孔的泡沫材料,最大可达?68%。随着细颗粒分数的增加,孔壁厚度显著减小。此外,所有模型均呈现出孔隙率最大值峰值,随着粒径比的增大,孔隙率峰值逐渐增大,并向低细粒率偏移。在低粒径比的实验泡沫中也观察到这种行为。然而,对于较高的尺寸比,孔隙率表现出归因于混合过程的不规则行为。
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引用次数: 2
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Theoretical and Applied Mechanics
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