南京航空航天大学学报（英文版）2016，Vol.33Issue(2)：129-136,8.
Jet Noise Reduction of Double-Mixing Exhaust System
Jet Noise Reduction of Double-Mixing Exhaust System
Shao Wanren 1Wu Fei 1He Jingyu 2Li Xiaodong3
作者信息
- 1. Shenyang Engine Design and Research Institute, Aviation Industry Corporation of China,Shenyang 110015, P.R.China
- 2. China Academy of Aerospace Aerodynamics,Beijing 100074, P.R.China
- 3. School of Energy and Power Engineering, Beihang University, Beijing 100191, P.R.China
- 折叠
摘要
关键词
aerospace propulsion system/high-bypass-ratio turbofan engine/mixing exhaust system/lobed mixer/chevron nozzle/jet noise reductionKey words
aerospace propulsion system/high-bypass-ratio turbofan engine/mixing exhaust system/lobed mixer/chevron nozzle/jet noise reduction分类
通用工业技术引用本文复制引用
Shao Wanren,Wu Fei,He Jingyu,Li Xiaodong..Jet Noise Reduction of Double-Mixing Exhaust System[J].南京航空航天大学学报（英文版）,2016,33(2):129-136,8.
