Numerical simulation of two dimension iced airfoil using immersed boundary method

被引：0
|
作者：
Zhong, Guo-Hua [1 ]
Sun, Xiao-Feng [1 ]
机构：
[1] School of Jet Propulsion, Beijing University of Aeronautics and Astronautics, Beijing 100191, China
来源：
Hangkong Dongli Xuebao/Journal of Aerospace Power | 2009年 / 24卷 / 08期
关键词：
Navier Stokes equations - Numerical methods - Turbulent flow - Numerical models - Computational fluid dynamics - Turbulence models;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
An immersed boundary method was applied to numerical simulation of the flow past a clean/iced NACA0012 airfoil. In this paper, two dimension imcompressible Reynolds-averaged Navier-Stokes equations were solved with SIMPLEC method. One equation turbulence model-Spalart-Allmaras turbulence model, was used in the numerical procedure. Good agreement was found between the present numerical results and previous experimental work.
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页码：1752 / 1758
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