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Numerical Investigation of an Oscillating Airfoil using Immersed Boundary Method

Guohua Zhong Lin Du Xiaofeng Sun

热科学学报（英文版）2011，Vol.20Issue(5)：413-422,10.

热科学学报（英文版）2011，Vol.20Issue(5)：413-422,10.DOI:10.1007/s11630-011-0489-y

Numerical Investigation of an Oscillating Airfoil using Immersed Boundary Method

Guohua Zhong ¹Lin Du ²Xiaofeng Sun²

作者信息

1. Aviation China Engineering, General Electric Co., Shanghai 201203, China
2. School of Jet Propulsion, Beihang University, Beijing 10019 1, China
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摘要

关键词

turbomachinery/IB method/fluid-structure interaction

Key words

turbomachinery/IB method/fluid-structure interaction

引用本文复制引用

Guohua Zhong,Lin Du,Xiaofeng Sun..Numerical Investigation of an Oscillating Airfoil using Immersed Boundary Method[J].热科学学报（英文版）,2011,20(5):413-422,10.

基金项目

This work was supported by NSFC under grants 50736007 and 50136010. （）

热科学学报（英文版）

OACSCDEISCI

ISSN：1003-2169

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