Development of the wind tunnel balance measuring for tiny roll moment with gas bearing

被引:0
|
作者
Wang, Shu-Min
Xie, Bin
Liu, Wei
机构
来源
| 2002年 / Zhongguo Kongqi Dongli Yanjiu yu Fazhan Zhongxin卷 / 16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
相关论文
共 19 条
  • [1] Hinge moment balance technique and application in hypersonic wind tunnel
    Xiong, Lin
    Liu, Zhan
    Chen, He-Wu
    Shiyan Liuti Lixue/Journal of Experiments in Fluid Mechanics, 2007, 21 (03): : 54 - 57
  • [2] Wind Tunnel Balance Development for Ludwieg Tube Facilities
    Simmons, Daniel J.
    Gothard, William D.
    Molinaro, Nicholas J.
    Meritt, Ryan J.
    AIAA AVIATION FORUM AND ASCEND 2024, 2024,
  • [3] Measuring Gas Concentration and Wind Intensity in a Turbulent Wind Tunnel with a Mobile Robot
    Martinez, Dani
    Moreno, Javier
    Tresanchez, Marcel
    Clotet, Eduard
    Manuel Jimenez-Soto, Juan
    Magrans, Rudys
    Pardo, Antonio
    Marco, Santiago
    Palacin, Jordi
    JOURNAL OF SENSORS, 2016, 2016
  • [4] Hinge moment balance technique with axial force measurement and its application in wind tunnel test
    Liu, Xi-He
    Wang, Tian-Hao
    Qiu, Jun-Wen
    Li, Sheng-Wen
    Feng, Xin-Hua
    Shiyan Liuti Lixue/Journal of Experiments in Fluid Mechanics, 2011, 25 (02): : 88 - 91
  • [5] A new force-measuring balance for large-scale model in hypersonic wind tunnel
    Wang, Qinchao
    Li, Shichao
    Gao, Hongli
    Lv, Jinzhou
    Zhang, Xiaoqin
    Liu, Weixiong
    Liu, Zihao
    REVIEW OF SCIENTIFIC INSTRUMENTS, 2021, 92 (11):
  • [6] NEW ROTATION-BALANCE APPARATUS FOR MEASURING AIRPLANE SPIN AERODYNAMICS IN THE WIND-TUNNEL
    MALCOLM, GN
    JOURNAL OF AIRCRAFT, 1979, 16 (04): : 264 - 268
  • [7] Prediction Interval Development for Wind-Tunnel Balance Check-Loading
    Landman, Drew
    Toro, Kenneth G.
    Commo, Sean A.
    Lynn, Keith C.
    JOURNAL OF AIRCRAFT, 2015, 52 (03): : 884 - 889
  • [8] The development of the larger axial force intermediate temperature balance in the hypersonic wind tunnel
    China Aerodynamics Research and Development Centre, Mianyang 621000, China
    Shiyan Liuti Lixue, 2006, 1 (86-90):
  • [9] Prediction interval development for wind-tunnel balance check-loading
    1600, AIAA International, 12700 Sunrise Valley Drive, Suite 200Reston, VA, Virginia, Virginia 20191-5807, United States (52):
  • [10] Development of a six-axis force/moment sensor for wind tunnel model test
    Wang, Wenjun
    MEASUREMENT SCIENCE AND TECHNOLOGY, 2013, 24 (11)