具有迭代Brinkman惩罚的涡质点法模拟尖形状物体的流动

IF 1.5 4区 工程技术 Q2 ENGINEERING, AEROSPACE
V. D. Duong, L. Zuhal
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引用次数: 1

摘要

本文提出了一种拉格朗日涡旋法和迭代Brinkman惩罚相结合的方法,用于模拟通过复杂几何体的不可压缩流。在所提出的算法中,分别引入了粒子域和惩罚域。粒子域用于计算粒子对流和扩散,而惩罚域用于强制执行壁边界条件。在迭代Brinkman惩罚中,通过在每个时间步长内多次施加惩罚力来强制执行无滑移边界条件。这使得大的时间步长能够降低计算成本,并保持处理复杂几何形状的能力。该方法已针对基准问题进行了验证,例如通过圆柱、垂直于平板的脉冲启动流,以及雷诺数在550至1000之间的对称翼型。涡度和流线等值线、阻力和升力系数与文献报道的结果一致。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Vortex particle method with iterative Brinkman penalization for simulation of flow past sharp-shape bodies
This paper presents a Lagrangian vortex method combined with iterative Brinkman penalization for the simulation of incompressible flow past a complex geometry. In the proposed algorithm, particle and penalization domains are separately introduced. The particle domain is for the computation of particle convection and diffusion, while the penalization domain is the enforcement of the wall boundary conditions. In iterative Brinkman penalization, the no-slip boundary condition is enforced by applying penalization force in multiple times within each time step. This enables large time step size reducing computational cost and maintains the capability in handling complex geometries. The method is validated for benchmark problems such as an impulsively started flow past a circular cylinder, normal to a flat plate, and a symmetric airfoil at Reynolds numbers ranging from 550 to 1000. The vorticity and streamline contours, drag, and lift coefficients show a good agreement with those reported in literature.
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来源期刊
CiteScore
3.00
自引率
7.10%
发文量
13
审稿时长
>12 weeks
期刊介绍: The role of the International Journal of Micro Air Vehicles is to provide the scientific and engineering community with a peer-reviewed open access journal dedicated to publishing high-quality technical articles summarizing both fundamental and applied research in the area of micro air vehicles.
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