Immersed Boundary Method on Deformable Unstructured Meshes for Airfoil Aeroacoustic Simulation

被引：0
作者：
I. V. Abalakin
A. P. Duben
N. S. Zhdanova
T. K. Kozubskaya
L. N. Kudryavtseva
机构：
[1] Federal Research Center Keldysh Institute of Applied Mathematics,
[2] Russian Academy of Sciences,undefined
[3] Dorodnicyn Computing Center,undefined
[4] Federal Research Center “Computer Science and Control,undefined
[5] ” Russian Academy of Sciences,undefined
来源：
Computational Mathematics and Mathematical Physics | 2019年 / 59卷
关键词：
immersed boundary method; Brinkman penalization method; unstructured mesh; moving mesh; mesh deformation; LES approach; turbulent flow; airfoil; slat; aeroacoustics;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：1982 / 1993
页数：11
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