Direct Numerical Simulation of Supersonic Turbulent Boundary Layer with Spanwise Wall Oscillation

Direct Numerical Simulation of Supersonic Turbulent Boundary Layer with Spanwise Wall Oscillation

Direct numerical simulations (DNS) of Mach = 2.9 supersonic turbulent boundary layers with spanwise wall oscillation (SWO) are conducted to investigate the turbulent heat transport mechanism and its relation with the turbulent momentum transport. The turbulent coherent structures are suppressed by S...

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Bibliographic Details
Main Authors: Weidan Ni, Lipeng Lu, Catherine Le Ribault, Jian Fang
Format: Article
Language:English
Published: MDPI AG 2016-03-01
Series:Energies
Subjects:
direct numerical simulation
turbulent heat transport
wall heat flux
spanwise wall oscillation
Online Access:http://www.mdpi.com/1996-1073/9/3/154

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http://www.mdpi.com/1996-1073/9/3/154

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