F-16 FLUTTER SUPPRESSION SYSTEM INVESTIGATION FEASIBILITY STUDY AND WIND-TUNNEL TESTS

被引：5
|
作者：
PELOUBET, RP
HALLER, RL
BOLDING, RM
机构：
来源：
JOURNAL OF AIRCRAFT | 1982年 / 19卷 / 02期
关键词：
D O I：
10.2514/3.57371
中图分类号：
V [航空、航天];
学科分类号：
08 ; 0825 ;
摘要：
引用
收藏
页码：169 / 175
页数：7
相关论文
共 50 条
  • [1] Robust Flutter Suppression and Wind-Tunnel Tests of a Three-Dimensional Wing
    Qian, Wenmin
    JOURNAL OF AEROSPACE ENGINEERING, 2018, 31 (06)
  • [2] Design of active flutter suppression and wind-tunnel tests of a wing model involving a control delay
    Huang, Rui
    Qian, Wenmin
    Hu, Haiyan
    Zhao, Yonghui
    JOURNAL OF FLUIDS AND STRUCTURES, 2015, 55 : 409 - 427
  • [3] FLUTTER AND OSCILLATORY PRESSURE TESTS ON A 727 AILERON IN A WIND-TUNNEL
    NAGARAJA, KS
    LAKIN, GC
    BARTLEY, JB
    JOURNAL OF AIRCRAFT, 1982, 19 (09): : 781 - 786
  • [4] Wind-Tunnel Tests for Active Flutter Control and Closed-Loop Flutter Identification
    Huang, Rui
    Zhao, Yonghui
    Hu, Haiyan
    AIAA JOURNAL, 2016, 54 (07) : 2089 - 2099
  • [5] WIND-TUNNEL STUDY OF THE FLUTTER CHARACTERISTICS OF A SUPERCRITICAL WING
    HOUWINK, R
    KRAAN, AN
    ZWAAN, RJ
    JOURNAL OF AIRCRAFT, 1982, 19 (05): : 400 - 405
  • [6] Hypersonic flutter and flutter suppression system of a wind tunnel model
    Chuanwei XUAN
    Jinglong HAN
    Bing ZHANG
    Haiwei YUN
    Xiaomao CHEN
    Chinese Journal of Aeronautics, 2019, 32 (09) : 2121 - 2132
  • [7] Hypersonic flutter and flutter suppression system of a wind tunnel model
    Chuanwei XUAN
    Jinglong HAN
    Bing ZHANG
    Haiwei YUN
    Xiaomao CHEN
    Chinese Journal of Aeronautics, 2019, (09) : 2121 - 2132
  • [8] Hypersonic flutter and flutter suppression system of a wind tunnel model
    Xuan, Chuanwei
    Han, Jinglong
    Zhang, Bing
    Yun, Haiwei
    Chen, Xiaomao
    CHINESE JOURNAL OF AERONAUTICS, 2019, 32 (09) : 2121 - 2132
  • [9] RECENT DEVELOPMENTS IN THE F-16 FLUTTER SUPPRESSION WITH ACTIVE CONTROL PROGRAM
    PELOUBET, RP
    HALLER, RL
    BOLDING, RM
    JOURNAL OF AIRCRAFT, 1984, 21 (09): : 716 - 721
  • [10] Experimental and Theoretical Flutter Investigation for a Range of Wing Wind-Tunnel Models
    Moradi, Mehrdad
    Sadeghi, Morteza H.
    Dowell, Earl H.
    JOURNAL OF AIRCRAFT, 2018, 55 (02): : 891 - U12
12345