Airworthiness compliance validating technique for wind tunnel test of a civil aircraft low speed flutter model

被引：0
|
作者：
Liang, Ji [1 ]
Yang, Fei [1 ]
Yang, Zhi-Chun [1 ]
机构：
[1] Stress Department, Shanghai Aircraft Design and Research Institute of COMAC, Shanghai 200232, China
来源：
Zhendong yu Chongji/Journal of Vibration and Shock | 2013年 / 32卷 / 12期
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：1 / 5
相关论文
共 50 条
  • [21] Model Updating and Aeroelastic Correlation of a Scaled Wind Tunnel Model for Active Flutter Suppression Test
    Di Leone, Domenico
    Lo Balbo, Francesco
    De Gaspari, Alessandro
    Ricci, Sergio
    AEROSPACE, 2021, 8 (11)
  • [22] Study on the method of test and control system for low speed wind tunnel
    Yang, Yueming
    Luo, Kai
    Bao, Xingrong
    Li, Yuankai
    PROCEEDINGS OF THE 2015 INTERNATIONAL CONFERENCE ON AUTOMATION, MECHANICAL CONTROL AND COMPUTATIONAL ENGINEERING, 2015, 124 : 1970 - 1974
  • [23] FERA in parameter identification with application in low speed wind tunnel test
    Huang, Ching-Huei
    Lin, Chun-Liang
    Chao, Maw-Jy
    AEROSPACE SCIENCE AND TECHNOLOGY, 2011, 15 (06) : 495 - 509
  • [24] Low speed wind tunnel moving ground test bed design
    Edzierski, Lukasz K.
    Krysztofiak, Grzegorz
    Praski, Radoslaw
    Podlevski, Edvin
    Kapuscinski, Jakub
    Liberacki, Adam
    Miller, Marek
    Osiewicz, Maciej
    FLOW MEASUREMENT AND INSTRUMENTATION, 2024, 96
  • [25] Bifurcation Behavior of Airfoil Undergoing Stall Flutter Oscillations in Low-Speed Wind Tunnel
    Dimitriadis, Grigorios
    Li, Jing
    AIAA JOURNAL, 2009, 47 (11) : 2577 - 2596
  • [26] The test technique for aircraft with high aspect ratio in the 2.4 meter transonic wind tunnel
    Chen, De-Hua
    Yin, Lu-Ping
    Wu, Wen-Hua
    Li, Jian-Qiang
    Shi, Jian-Yuan
    Peng, Yun
    Kongqi Donglixue Xuebao/Acta Aerodynamica Sinica, 2009, 27 (05): : 542 - 546
  • [27] Design of Scale Model Mechanism in Low Speed Wind Tunnel
    AHMAD Aldarouich
    Computer Aided Drafting,Design and Manufacturing, 2008, Design and Manufacturing.2008 (02) : 57 - 64
  • [28] Non-intrusive test technique investigation of transition measurement with infrared image in low speed wind tunnel
    Geng, Zi-Hai
    He, Xian-Zhong
    Wang, Xun-Nian
    Chen, Peng
    Zhang, Yang
    Shiyan Liuti Lixue/Journal of Experiments in Fluid Mechanics, 2010, 24 (06): : 77 - 82
  • [29] Flight Mechanics Test with a Restricted Flying Aircraft Model in a Wind Tunnel.
    Subke, Henning
    Forschungsbericht - Deutsche Forschungs-und Versuchsanstalt fuer Luft-und Raumfahrt, 1984,
  • [30] A novel forecasting method of flutter critical wind speed for the 15 MW wind turbine blade based on aeroelastic wind tunnel test
    Lu, Man-man
    Ke, Shi-tang
    Wu, Hong-xin
    Tian, Wen-xin
    Wang, Hao
    Gao, Mu-en
    JOURNAL OF WIND ENGINEERING AND INDUSTRIAL AERODYNAMICS, 2022, 230
12345