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Rotor Airload and Acoustics Prediction Based on CFD/CSD Coupling Method

Wang Liangquan Xu Guohua Shi Yongjie

南京航空航天大学学报（英文版）2018，Vol.35Issue(2)：343-352,10.
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南京航空航天大学学报（英文版）2018，Vol.35Issue(2)：343-352,10.

Rotor Airload and Acoustics Prediction Based on CFD/CSD Coupling Method

Rotor Airload and Acoustics Prediction Based on CFD/CSD Coupling Method

Wang Liangquan 1Xu Guohua 1Shi Yongjie1

作者信息

  • 1. National Key Laboratory of Science and Technology on Rotorcraft Aeromechanics,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,P.R.China
  • 折叠

摘要

关键词

helicopter/rotor/airload/aerodynamic noise/computational fluid dynamics(CFD)/computational structural dynamics(CSD)

Key words

helicopter/rotor/airload/aerodynamic noise/computational fluid dynamics(CFD)/computational structural dynamics(CSD)

分类

航空航天

引用本文复制引用

Wang Liangquan,Xu Guohua,Shi Yongjie..Rotor Airload and Acoustics Prediction Based on CFD/CSD Coupling Method[J].南京航空航天大学学报（英文版）,2018,35(2):343-352,10.

基金项目

This work was supported by Funding of Jiangsu Inno-vation Program for Graduate Education(No.KYLX16_0389). （No.KYLX16_0389）

南京航空航天大学学报（英文版）

OACSCDCSTPCD

1005-1120

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