Direct numerical simulation of hypersonic turbulent boundary layers: effect of spatial evolution and Reynolds number
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Publication:5861624
DOI10.1017/jfm.2022.80OpenAlexW4214633120MaRDI QIDQ5861624
Meelan M. Choudhari, Lian Duan, Junji Huang
Publication date: 1 March 2022
Published in: Journal of Fluid Mechanics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1017/jfm.2022.80
Related Items (11)
Wall-cooling effects on pressure fluctuations in compressible turbulent boundary layers from subsonic to hypersonic regimes ⋮ Linear response analysis of supersonic turbulent channel flows with a large parameter space ⋮ Study of the linear models in estimating coherent velocity and temperature structures for compressible turbulent channel flows ⋮ Conditional analysis on extreme wall shear stress and heat flux events in compressible turbulent boundary layers ⋮ Wall cooling effect on spectra and structures of thermodynamic variables in hypersonic turbulent boundary layers ⋮ Compressibility effects in supersonic and hypersonic turbulent boundary layers subject to wall disturbances ⋮ Reynolds number and wall cooling effects on correlations between the thermodynamic variables in hypersonic turbulent boundary layers ⋮ Linear-model-based study of the coupling between velocity and temperature fields in compressible turbulent channel flows ⋮ Effect of bulk viscosity on the hypersonic compressible turbulent boundary layer ⋮ Natural grid stretching for DNS of compressible wall-bounded flows ⋮ Total and static temperature statistics in compressible turbulent plane channel flow
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