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Experimental study on the boundary layer transition of a high-speed fin-cone configuration

Xueliang Li Binghui Xu Ganglei Huang Jie Wu

Advances in Aerodynamics2025,Vol.7Issue(2):P.80-96,17.
Advances in Aerodynamics2025,Vol.7Issue(2):P.80-96,17.DOI:10.1186/s42774-025-00204-9

Experimental study on the boundary layer transition of a high-speed fin-cone configuration

Xueliang Li 1Binghui Xu 2Ganglei Huang 3Jie Wu1

作者信息

  • 1. School of Aerospace Engineering,Huazhong University of Science and Technology,Wuhan 430074,China
  • 2. School of Artificial Intelligence and Automation,Huazhong University of Science and Technology,Wuhan 430074,China
  • 3. State Key Laboratory of Aerodynamics,Mianyang 621000,China
  • 折叠

摘要

关键词

High-speed boundary layer/Transition/Fin-cone configuration/FLDI/Second-mode instabilities

分类

航空航天

引用本文复制引用

Xueliang Li,Binghui Xu,Ganglei Huang,Jie Wu..Experimental study on the boundary layer transition of a high-speed fin-cone configuration[J].Advances in Aerodynamics,2025,7(2):P.80-96,17.

基金项目

supported by an Experimental Identification Technology Research Project(No.2022G02000250007). (No.2022G02000250007)

Advances in Aerodynamics

2097-3462

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