您当前的位置:
首页 >
文章列表页 >
Numerical simulation of hypersonic magnetofluid control based on non-linear coupling constitutive relation
更新时间:2026-05-28
    • Numerical simulation of hypersonic magnetofluid control based on non-linear coupling constitutive relation

    • Vol. 44, Issue 2, Pages: 68-80(2026)
    • DOI:10.7638/kqdlxxb-2024.0160    

      CLC: V231;V411.4;O361.3
    • Published:2026

    移动端阅览

  • Shi Hao, Xiao Hong, Zhou Li, et al. Numerical simulation of hypersonic magnetofluid control based on non-linear coupling constitutive relation[J]. 2026, 44(2): 68-80. DOI: 10.7638/kqdlxxb-2024.0160.

  •  
  •  
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

The influence of adjustable slot configuration on aerodynamic characteristics of airfoil
Numerical and experimental study on opposing jet in hypersonic flow
Stall characteristics of high-lift device improved by slotting on leading-edge slat
Numerical simulation of flow control in lift-increase effect using air-blowing
Impact of key area optimization on the aerodynamic characteristics of a high-speed train in crosswind

Related Author

LYU Wenhao
ZHANG Zhihao
HAO Lishu
GAO Yongwei
DONG Hao
ZHANG Xudong
LIU Shicheng
CHENG Keming

Related Institution

Unmanned Systems Research Institute, Northwestern Polytechnical University, Xi 'an
National Key Laboratory of Science and Technology on Aerodynamic Design and Research, Northwestern Polytechnical University, Xi 'an
College of Aerospace Engineering, Nanjing University of Aeronautics And Astronautics, Nanjing
Key Laboratory of Unsteady Aerodynamics and Flow Control, Ministry of Industry and Information Technology, Nanjing
Computational Aerodynamics Institute of China Aerodynamics Research and Development Center, Mianyang
0