A design method of the static aeroelastic aircraft model based on stereolithgraphy for wind tunnel test

被引:0
|
作者
机构
[1] [1,Wang, Chao
[2] Zhang, Zhengyu
[3] Yin, Guofu
[4] Sun, Yan
[5] Zhu, Weijun
来源
Wang, C. (superwln@qq.com) | 1600年 / Chinese Society of Astronautics卷 / 35期
关键词
Fabrication;
D O I
10.7527/S1000-6893.2013.0415
中图分类号
学科分类号
摘要
引用
收藏
相关论文
共 50 条
  • [1] Wind Tunnel Model Static Aeroelastic Deformation Correction Method Based on Grid Reconstruction
    Chen Kai
    Cheng Pan
    Mao Kun
    Chen Ying
    Wu Dawei
    2023 ASIA-PACIFIC INTERNATIONAL SYMPOSIUM ON AEROSPACE TECHNOLOGY, VOL I, APISAT 2023, 2024, 1050 : 927 - 936
  • [2] Separation method for Reynolds number/static aeroelastic coupling effect in wind tunnel test
    Guo Q.
    Sun Y.
    Guo Z.
    Liu G.
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2022, 43 (11):
  • [3] Design and fabrication of an aircraft static aeroelastic model based on rapid prototyping
    Wang, Chao
    Yin, Guofu
    Zhang, Zhengyu
    Wang, Shuiliang
    Zhao, Tao
    Sun, Yan
    Yang, Dangguo
    RAPID PROTOTYPING JOURNAL, 2015, 21 (01) : 34 - 42
  • [4] Static Aeroelastic Analysis of an Aircraft Wind-Tunnel Model by Means of Modal RBF Mesh Updating
    Biancolini, Marco Evangelos
    Cella, Ubaldo
    Groth, Corrado
    Genta, Massimiliano
    JOURNAL OF AEROSPACE ENGINEERING, 2016, 29 (06)
  • [5] Design of aeroelastic model of large-span stadium roof and wind tunnel test
    Gu, Ming
    Huang, Xiang
    Jianzhu Jiegou Xuebao/Journal of Building Structures, 2005, 26 (01): : 60 - 64
  • [6] The Design, Manufacture and Wind Tunnel Test of the Full Aircraft Transonic Flutter Model
    Wei, Qian
    De, Guan
    EMERGING MATERIALS AND MECHANICS APPLICATIONS, 2012, 487 : 267 - +
  • [7] Wind tunnel model flight test technique for advanced fighter aircraft design
    Cen F.
    Nie B.
    Liu Z.
    Guo L.
    Sun H.
    Li Q.
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2020, 41 (06):
  • [8] Wind vibration characteristics of high-rise masts based on aeroelastic model wind tunnel test
    Liu M.
    Du R.
    Xie Z.
    1600, Southeast University (54): : 861 - 869
  • [9] Wind Tunnel Model Design and Aeroelastic Measurements of the RIBES Wing
    Cella, Ubaldo
    Della Vecchia, Pierluigi
    Groth, Corrado
    Porziani, Stefano
    Chiappa, Andrea
    Giorgetti, Francesco
    Nicolosi, Fabrizio
    Biancolini, Marco Evangelos
    JOURNAL OF AEROSPACE ENGINEERING, 2021, 34 (01)
  • [10] Design and wind tunnel test of a MODular aeroelastic FLEXible wing (MODFLEX)
    Fichera, S.
    Jiffri, S.
    Mottershead, J. E.
    PROCEEDINGS OF ISMA2016 INTERNATIONAL CONFERENCE ON NOISE AND VIBRATION ENGINEERING AND USD2016 INTERNATIONAL CONFERENCE ON UNCERTAINTY IN STRUCTURAL DYNAMICS, 2016, : 445 - 456