Aerodynamic performance of rotor with new type blade-tip in hover based upon test and numerical investigations

被引：0
|
作者：
Zhao, Qijun [1 ]
Xu, Guohua [1 ]
机构：
[1] National Key Laboratory of Rotorcraft Aeromechanics, Nanjing University of Aeronautics and Astronautics, Nanjing 210016, China
来源：
Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica | 2009年 / 30卷 / 03期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
14
引用
收藏
页码：422 / 429
相关论文
共 50 条
  • [1] The primary experiments on aeroacoustic of rotor with unconventional blade-tip in hover
    Zhao, Qi-Jun
    Xu, Guo-Hua
    Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica, 2009, 27 (03): : 320 - 324
  • [2] Aerodynamic Performance and Aeroacoustic Characteristics of Model Rotor with Anhedral Blade Tip in Hover
    Huang, Shuilin
    Fan, Feng
    Yuan, Mingchuan
    Sun, Wei
    Transactions of Nanjing University of Aeronautics and Astronautics, 2018, 35 (01) : 162 - 169
  • [3] Aerodynamic Performance and Aeroacoustic Characteristics of Model Rotor with Anhedral Blade Tip in Hover
    Huang Shuilin
    Fan Feng
    Yuan Mingchuan
    Sun Wei
    TransactionsofNanjingUniversityofAeronauticsandAstronautics, 2018, 35 (01) : 162 - 169
  • [4] Assessment of Tip Shape Effect on Rotor Aerodynamic Performance in Hover
    Hwang, Je Young
    Kwon, Oh Joon
    INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2015, 16 (02) : 295 - 310
  • [5] Numerical optimization of helicopter rotor aerodynamic performance in hover
    Le Pape, A
    Beaumier, P
    AEROSPACE SCIENCE AND TECHNOLOGY, 2005, 9 (03) : 191 - 201
  • [6] Effects of the rotor tip gap on the aerodynamic and aeroacoustic performance of a ducted rotor in hover
    Goudswaard, Reinier J.
    Ragni, Daniele
    Baars, Woutijn J.
    AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 155
  • [7] Overtip Choking and Its Implications on Turbine Blade-Tip Aerodynamic Performance
    Zhang, Q.
    He, L.
    JOURNAL OF PROPULSION AND POWER, 2011, 27 (05) : 1008 - 1014
  • [8] Structural Parameter Analyses on Rotor Airloads with New Type Blade-Tip Based on CFD/CSD Coupling Method
    Wang Junyi
    Zhao Qijun
    Ma Li
    Transactions of Nanjing University of Aeronautics and Astronautics, 2016, 33 (06) : 678 - 686
  • [9] Experiment of hover performance with new shape blade tip
    Sun, Chuan-Wei
    Lu, Yang
    Gao, Zheng
    Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica, 2001, 19 (04):
  • [10] Numerical study of aerodynamic characteristics of darrieus wind turbine with blade-tip end plates
    University of Shanghai for Science and Technology, Shanghai
    200093, China
    不详
    200093, China
    不详
    314051, China
    Kung Cheng Je Wu Li Hsueh Pao, 9 (1922-1926):
12345