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题名

Compressibility effect in hypersonic boundary layer with isothermal wall condition

作者
通讯作者Wang, Jianchun
发表日期
2021-05-24
DOI
发表期刊
ISSN
2469-990X
卷号6期号:5
摘要

The compressibility effect in isothermal hypersonic boundary layer is studied with direct numerical simulation (DNS) using Helmholtz decomposition. The dilatational components of the diagonal Reynolds stress are enhanced by the cold wall condition in the near-wall region. The outward (Q1) and ejection (Q2) events are mainly located in the expansion region, while the inward (Q3) and sweep (Q4) events are primarily situated in the compression region near the wall. It is found that the cold wall condition can enhance the inward (Q3) event mainly in the compression region and enhance the ejection (Q2) event mainly in the expansion region near the wall. In particular, the cold wall can significantly enhance the positive streamwise solenoidal fluctuating velocity and negative wall-normal dilatational fluctuating velocity events. Moreover, the cold wall condition enhances the positive correlation of streamwise velocity fluctuation and fluctuating temperature, and suppresses the negative correlation of wall-normal velocity fluctuation and fluctuating temperature in the near-wall region, while it slightly weakens the negative correlation of streamwise velocity fluctuation and fluctuating temperature and the positive correlation of wall-normal velocity fluctuation and fluctuating temperature far from the wall. It is also found that the dilatational components of correlations are dominated in the near-wall region, while the solenoidal components govern the correlations far from the wall. Most of the interactions among mean and fluctuating fields of kinetic and internal energy are governed by the solenoidal components, except for the terms associated with the pressure, which are governed by the dilatational components.

相关链接[来源记录]
收录类别
SCI ; EI
语种
英语
学校署名
通讯
资助项目
NSFC Basic Science Center Program[11988102]
WOS研究方向
Physics
WOS类目
Physics, Fluids & Plasmas
WOS记录号
WOS:000655981700001
出版者
EI入藏号
20212310466529
EI主题词
Compressibility ; Expansion ; Hypersonic flow ; Isotherms ; Reynolds number ; Solenoids ; Velocity
EI分类号
Fluid Flow, General:631.1 ; Electric Components:704.1 ; Materials Science:951
来源库
Web of Science
引用统计
被引频次[WOS]:27
成果类型期刊论文
条目标识符http://kc.sustech.edu.cn/handle/2SGJ60CL/229437
专题工学院_力学与航空航天工程系
作者单位
1.Peking Univ, Coll Engn, State Key Lab Turbulence & Comple Syst, Beijing 100871, Peoples R China
2.Southern Univ Sci & Technol, Dept Mech & Aerosp Engn, Ctr Complex Flows & Soft Matter Res, Guangdong Prov Key Lab Fundamental Turbulence Res, Shenzhen 518055, Peoples R China
3.Chinese Acad Sci, Inst Mech, Lab High Temp Gas Dynam, Beijing 100190, Peoples R China
通讯作者单位力学与航空航天工程系
推荐引用方式
GB/T 7714
Xu, Dehao,Wang, Jianchun,Wan, Minping,et al. Compressibility effect in hypersonic boundary layer with isothermal wall condition[J]. Physical Review Fluids,2021,6(5).
APA
Xu, Dehao,Wang, Jianchun,Wan, Minping,Yu, Changping,Li, Xinliang,&Chen, Shiyi.(2021).Compressibility effect in hypersonic boundary layer with isothermal wall condition.Physical Review Fluids,6(5).
MLA
Xu, Dehao,et al."Compressibility effect in hypersonic boundary layer with isothermal wall condition".Physical Review Fluids 6.5(2021).
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