您当前的位置:
首页 >
文章列表页 >
Modification of Spalart-Allmaras model with pressure gradientaiming for corner separation flow
更新时间:2026-07-07
    • Modification of Spalart-Allmaras model with pressure gradientaiming for corner separation flow

    • Vol. 31, Issue 10, Pages: 2405-2414(2016)
    • DOI:10.13224/j.cnki.jasp.2016.10.013    

      CLC:
    • Published:2016

    移动端阅览

  • doi: 10.13224/j.cnki.jasp.2016.10.013 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

525

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

Control of blade end slot on shock wave/boundary layer interaction of transonic cascade corner
Flow control mechanism of diffuser cascade corner-suction surface profiling design
Influence of S3 area ratio gradient at trailing edge on turbine rare frame
Effect of non-axisymmetric endwall on secondary flow in axial fan
Characteristics of bump induced curved shock/boundary layer interaction under the sideslip condition

Related Author

JI Lucheng
ZHOU Ling
MA Jianci
CUI Yiqiang
DONG Jiezhong
LI Xiangjun
GUI Xingmin
JIN Donghai

Related Institution

Institute for Aero Engine, Tsinghua University
School of Aerospace Engineering, Beijing Institute of Technology
北京航空航天大学 能源与动力工程学院
先进航空发动机协同创新研究中心
南京航空航天大学 能源与动力学院 江苏省航空动力系统重点实验室
0