振动NACA0012翼型的移动网格数值模拟

计算物理 ›› 2016, Vol. 33 ›› Issue (3): 266-272.

振动NACA0012翼型的移动网格数值模拟

曾现洋¹, 倪国喜²

1. 中国工程物理研究院研究生部, 北京 100088;
2. 计算物理实验室, 北京应用物理与计算数学研究所, 北京 100088

收稿日期:2015-03-19 修回日期:2015-05-31 出版日期:2016-05-25 发布日期:2016-05-25
作者简介:曾现洋(1973-),男,山东东平,副教授,硕士,从事计算流体力学方法研究,E-mail:mr.xyz@126.com
基金资助:
国家自然科学基金(91130020)与国防基础科研计划(B1520133015)资助项目

Moving Mesh Method for Pitching Naca0012 Airfoil

ZENG Xianyang¹, NI Guoxi²

1. Graduate School of China Academy of Engineering Physics, Beijing 100088, China;
2. Laboratory of Computational Physics, Institute of Applied Physics and Computational Mathematics, Beijing 100088, China

Received:2015-03-19 Revised:2015-05-31 Online:2016-05-25 Published:2016-05-25

摘要/Abstract

摘要： 利用流体力学方程的积分形式给出非结构移动网格上离散格式,利用自适应移动网格方法移动网格,进而得到网格速度.对振动Naca0012翼型问题,分三种类型确定网格速度,再结合Riemann问题的解法器构造数值通量,得到移动网格单元上新的物理量.数值实验表明这种格式同时具有高效、高分辨率的特点.

关键词: 可压流体力学方程, 运动边界, Naca0012翼型, 自适应移动网格方法

Abstract: We give discretization for fluid system in integral form with arbitrary moving velocity on unstructured meshes, where re-mapping step in ALE method to interpolate flow variables between old mesh and new one can be avoided. We give three kinds of velocity for different part of computational domain, and apply the scheme to pitching Naca0012 airfoil with moving boundary. It shows that the scheme is efficient and accurate.

Key words: compressible fluid system, moving boundary, pitching Naca0012, adaptive moving mesh method

中图分类号:

O351

曾现洋, 倪国喜. 振动NACA0012翼型的移动网格数值模拟[J]. 计算物理, 2016, 33(3): 266-272.

ZENG Xianyang, NI Guoxi. Moving Mesh Method for Pitching Naca0012 Airfoil[J]. CHINESE JOURNAL OF COMPUTATIONAL PHYSICS, 2016, 33(3): 266-272.

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