GUST RESPONSE OF ROTARY WING AIRCRAFT AND ITS ALLEVIATION

被引:0
|
作者
SAITO, S
AZUMA, A
NAGAO, M
机构
来源
VERTICA | 1981年 / 5卷 / 02期
关键词
D O I
暂无
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
HELICOPTERS
引用
收藏
页码:173 / 184
页数:12
相关论文
共 50 条
  • [1] Gust response and body freedom flutter of a flying-wing aircraft with a passive gust alleviation device
    Guo, S.
    Jing, Z. W.
    Li, H.
    Lei, W. T.
    He, Y. Y.
    AEROSPACE SCIENCE AND TECHNOLOGY, 2017, 70 : 277 - 285
  • [2] Gust load alleviation on an aircraft wing by trailing edge Circulation Control
    Li, Yonghong
    Qin, Ning
    JOURNAL OF FLUIDS AND STRUCTURES, 2021, 107
  • [3] Strategy for robust gust response alleviation of an aircraft model
    Dai, Yuting
    Yang, Chao
    Wang, Chaolei
    CONTROL ENGINEERING PRACTICE, 2017, 60 : 211 - 217
  • [4] Gust response alleviation of the aircraft wing aeroelastic systems in supersonic flows using nonlinear energy sink
    Niu, Yaobin
    Yang, Weiqi
    Huang, Wei
    AEROSPACE SCIENCE AND TECHNOLOGY, 2024, 155
  • [5] Comparison of the passive and active control gust alleviation of a flying-wing aircraft
    Liu, Ying
    JOURNAL OF ENGINEERING-JOE, 2019, (13): : 421 - 423
  • [6] Experimental and numerical investigation of an aircraft wing with hinged wingtip for gust load alleviation
    Balatti, Davide
    Khodaparast, Hamed Haddad
    Friswell, Michael I.
    Manolesos, Marinos
    Castrichini, Andrea
    JOURNAL OF FLUIDS AND STRUCTURES, 2023, 119
  • [7] Gust response modeling and alleviation scheme design for an elastic aircraft
    WU ZhiGang1
    2 The First Institute
    Science China(Technological Sciences), 2010, (11) : 3110 - 3118
  • [8] Gust response modeling and alleviation scheme design for an elastic aircraft
    Wu ZhiGang
    Chen Lei
    Yang Chao
    Tang ChangHong
    SCIENCE CHINA-TECHNOLOGICAL SCIENCES, 2010, 53 (11) : 3110 - 3118
  • [9] Gust response modeling and alleviation scheme design for an elastic aircraft
    ZhiGang Wu
    Lei Chen
    Chao Yang
    ChangHong Tang
    Science China Technological Sciences, 2010, 53 : 3110 - 3118
  • [10] Gust response modeling and alleviation scheme design for an elastic aircraft
    WU ZhiGang CHEN Lei YANG Chao TANG ChangHong School of Aeronautic Science and Engineering Beihang University Beijing China The First Institute Aviation Industry Corporation of China Xian China
    Science China(Technological Sciences), 2010, 53 (11) : 3110 - 3118