您当前的位置:
首页 >
文章列表页 >
Experimental study of aerodynamic characterictics of CHN-T1 standard model in 2.4 m transonic wind tunnel
更新时间:2026-05-28
    • Experimental study of aerodynamic characterictics of CHN-T1 standard model in 2.4 m transonic wind tunnel

    • Vol. 37, Issue 2, Pages: 337-344(2019)
    • DOI:10.7638/kqdlxxb-2018.0099    

      CLC: V211.7
    • Published:2019

    移动端阅览

  • LI Qiang, LIU Dawei, XU Xin, et al. Experimental study of aerodynamic characterictics of CHN-T1 standard model in 2.4 m transonic wind tunnel[J]. 2019, 37(2): 337-344. DOI: 10.7638/kqdlxxb-2018.0099.

  •  
  •  
icon
试读结束,您可以激活您的VIP账号继续阅读。
去激活 >
icon
试读结束,您可以通过登录账户,到个人中心,购买VIP会员阅读全文。
已是VIP会员?
去登录 >

0

Views

0

下载量

0

CSCD

Alert me when the article has been cited
提交
Tools
Download
Export Citation
Share
Add to favorites
Add to my album

Related Articles

Experimental investigation of vortex generator influence on wind turbine airfoil aerodynamic performance under turbulent inflow conditions
Aerodynamic characteristics simulation of CHN-T1 model with TRIP3.0
The study of interference characteristics of typical support struts on large aircraft in high-speed wind tunnels
Static aerodynamic characteristics of symmetrical wind turbine airfoils considering the influence of near-ocean underlying surface
Aerodynamic characteristics of combined wing-tip link UAV

Related Author

YANG Junwei
SHA Chenglong
WANG Xiangjun
YANG Hua
LI Wei
WANG Yuntao
HONG Junwu
MENG Dehong

Related Institution

Guangling College of Yangzhou University, Yangzhou
College of Electrical, Energy and Power Engineering, Yangzhou University, Yangzhou
Yancheng Technician College Jiangsu Province, Yancheng
College of Aeronautics and Astronautics, National University of Defense Technology
Computational Aerodynamic Institute of China Aerodynamics Research and Development Center
0