Numerical simulation of two dimension iced airfoil using immersed boundary method

ZHONG Guo-hua; SUN Xiao-feng

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Numerical simulation of two dimension iced airfoil using immersed boundary method

更新时间：2026-07-07

- Numerical simulation of two dimension iced airfoil using immersed boundary method
- Vol. 24, Issue 8, (2009)
- 作者机构：
  
  北京航空航天大学能源与动力工程学院,北京,100191
- 作者简介：
- 基金信息：
- DOI：
  CLC：
- Published：2009
- 稿件说明：
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ZHONG Guo-hua, SUN Xiao-feng. Numerical simulation of two dimension iced airfoil using immersed boundary method[J]. 2009, 24(8).
DOI：

ZHONG Guo-hua, SUN Xiao-feng. Numerical simulation of two dimension iced airfoil using immersed boundary method[J]. 2009, 24(8). DOI：

摘要

应用浸入式边界方法模拟干净/结冰NACA0012翼形绕流问题.采用SIMPLEC方法离散求解二维不可压雷诺平均Navier-Stokes方程

湍流模型采用一方程Spalart-Allmaras模型.计算结果与以往的实验结果吻合得很好

证明了浸入式边界方法和所发展的程序的可靠性.

Abstract

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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