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首页|期刊导航|Journal of Thermal Science|Shock Wave Spectrum Forming around the Compound Five-Hole Probe and its Influence on Pneumatic Parameters Acquisition during Subsonic to Supersonic Flow

Shock Wave Spectrum Forming around the Compound Five-Hole Probe and its Influence on Pneumatic Parameters Acquisition during Subsonic to Supersonic Flow

KAN Xiaoxu SUO Licheng LEI Haodong WU Wanyang ZHONG Jingjun

Journal of Thermal Science2024,Vol.33Issue(6):P.2019-2031,13.
Journal of Thermal Science2024,Vol.33Issue(6):P.2019-2031,13.DOI:10.1007/s11630-024-2047-4

Shock Wave Spectrum Forming around the Compound Five-Hole Probe and its Influence on Pneumatic Parameters Acquisition during Subsonic to Supersonic Flow

KAN Xiaoxu 1SUO Licheng 1LEI Haodong 1WU Wanyang 1ZHONG Jingjun1

作者信息

  • 1. Merchant Marine College,Shanghai Maritime University,Shanghai 201306,China
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摘要

关键词

pneumatic probes/supersonic flow/shock wave/pneumatic parameter/numerical simulation

分类

航空航天

引用本文复制引用

KAN Xiaoxu,SUO Licheng,LEI Haodong,WU Wanyang,ZHONG Jingjun..Shock Wave Spectrum Forming around the Compound Five-Hole Probe and its Influence on Pneumatic Parameters Acquisition during Subsonic to Supersonic Flow[J].Journal of Thermal Science,2024,33(6):P.2019-2031,13.

基金项目

co-supported by the National Natural Science Foundation of China(No.52236005) (No.52236005)

the Science Center for GasTurbineProject(No.P2022-B-II-007-001) (No.P2022-B-II-007-001)

the National Key Laboratory Funds(No.D5150230002). (No.D5150230002)

Journal of Thermal Science

OAEI

1003-2169

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