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Research on Aerodynamic Characteristics of Hovering Rotor Based on Leading Edge Droop

LI Congcong SHI Yongjie XU Guohua MA Taihang

南京航空航天大学学报：英文版2021，Vol.38Issue(S01)：P.10-16,7.

南京航空航天大学学报：英文版2021，Vol.38Issue(S01)：P.10-16,7.DOI:10.16356/j.1005-1120.2021.S.002

Research on Aerodynamic Characteristics of Hovering Rotor Based on Leading Edge Droop

LI Congcong ¹SHI Yongjie ²XU Guohua ²MA Taihang²

作者信息

1. Shanghai Aircraft Design and Research Institute,Shanghai 201210,P.R.China National Key Laboratory of Science and Technology on Rotorcraft Aerodynamics,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,P.R.China
2. National Key Laboratory of Science and Technology on Rotorcraft Aerodynamics,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,P.R.China
折叠

摘要

关键词

helicopter rotor/hovering/leading edge droop/aerodynamic characteristics

分类

航空航天

引用本文复制引用

LI Congcong,SHI Yongjie,XU Guohua,MA Taihang..Research on Aerodynamic Characteristics of Hovering Rotor Based on Leading Edge Droop[J].南京航空航天大学学报：英文版,2021,38(S01):P.10-16,7.

基金项目

supported by the National Natural Science Foundation of China(No.11972190) （No.11972190）

the Aeronautical Science Foundation of China(No. 20185752) （No. 20185752）

南京航空航天大学学报：英文版

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ISSN：1005-1120

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