您当前的位置:
首页 >
文章列表页 >
Development of liquid nitrogen supplying system of 0.3 m cryogenic wind tunnel
更新时间:2026-07-07
    • Development of liquid nitrogen supplying system of 0.3 m cryogenic wind tunnel

    • Vol. 35, Issue 5, Pages: 1009-1017(2020)
    • DOI:10.13224/j.cnki.jasp.2020.05.013    

      CLC:
    • Published:2020

    移动端阅览

  • doi: 10.13224/j.cnki.jasp.2020.05.013 DOI:

  •  
  •  
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

380

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

Simulation of water hammer in liquid nitrogen supplying system based on AMESim
Effect of condensation phase transient on Reynold number test for cryogenic wind tunnel
Internal heat transfer and skin temperature reduction law of engine nacelle
Orthogonal optimal design of solid fuel formulation for HO/HTPB hybrid rocket motor
与发动机匹配的旁路式双喉道气动矢量喷管数值模拟研究

Related Author

Wei ZHANG
Dewen SUN
Wanhua CHEN
Rong GAO
Jianye CHEN
Junlong XIE
Qian LIU
Heng XIE

Related Institution

Facility Design and Instrumentation Institute,China Aerodynamics Research and Development Center
College of Aerospace Science and Engineer,National University of Defense Technology
School of Energy and Power Engineering,Huazhong University of Science and Technology
Laboratory of Cryogenic Liquid Propellants,China Aerospace Science and Technology Corporation
Beijing Aerospace Propulsion Institute,China Aerospace Science and Technology Corporation
0