Turbulence in supersonic channel ow is studied using direct numerical simulation. The ability of outer and inner scalings to collapse proles of turbulent stresses onto their incompressible counterparts is investigated. Such collapse is adequate with outer scaling when suciently far from the wall, but not with inner scaling. Compressibility eects on the turbulent stresses, their anisotropy, and their balance equations are identied. A reduction in the near-wall pressure\u85strain, found responsible for the changed Reynolds-stress proles, is explained using a Greens-function-based analysis of the pressure eld. 1
The effect of Reynolds and Mach number variation in compressible isothermal channel flow is investi-...
When analyzing many turbulent flows, the effects of compressibility can be neglected. Even some rela...
This thesis presents the motivation, objectives and reasoning behind the undertaken PhD to investiga...
Direct numerical simulations of compressible turbulent channel flow including passive scalar transpo...
Several questions that are relevant to turbulence modeling are addressed on the basis of recently ob...
Compressible turbulent channel flows at two Mach numbers (M = 0.8 and 1.3) are simulated by the nume...
The present paper addresses some topical issues in modelling compressible turbulent shear flows. The...
A study of compressible supersonic turbulent flow in a plane channel with isothermal walls has been ...
The structure of the wall pressure field beneath supersonic adiabatic turbulent boundary layers is a...
Classical Mach-number (M) scaling in compressible wall turbulence was suggested by van Driest (Van D...
The relative scaling exponents and intermittency of three-dimensional compressible turbulent channel...
Mean flow and compressible turbulence measurements have been obtained upstream and within a shock bo...
177 p.Thesis (Ph.D.)--University of Illinois at Urbana-Champaign, 2001.Second, since it has been det...
Counter-flow configurations in a confined channel flow provide an efficient framework to study high ...
A scaling formula for the mean velocity and wall distance in compressible turbulent wall-bounded flo...
The effect of Reynolds and Mach number variation in compressible isothermal channel flow is investi-...
When analyzing many turbulent flows, the effects of compressibility can be neglected. Even some rela...
This thesis presents the motivation, objectives and reasoning behind the undertaken PhD to investiga...
Direct numerical simulations of compressible turbulent channel flow including passive scalar transpo...
Several questions that are relevant to turbulence modeling are addressed on the basis of recently ob...
Compressible turbulent channel flows at two Mach numbers (M = 0.8 and 1.3) are simulated by the nume...
The present paper addresses some topical issues in modelling compressible turbulent shear flows. The...
A study of compressible supersonic turbulent flow in a plane channel with isothermal walls has been ...
The structure of the wall pressure field beneath supersonic adiabatic turbulent boundary layers is a...
Classical Mach-number (M) scaling in compressible wall turbulence was suggested by van Driest (Van D...
The relative scaling exponents and intermittency of three-dimensional compressible turbulent channel...
Mean flow and compressible turbulence measurements have been obtained upstream and within a shock bo...
177 p.Thesis (Ph.D.)--University of Illinois at Urbana-Champaign, 2001.Second, since it has been det...
Counter-flow configurations in a confined channel flow provide an efficient framework to study high ...
A scaling formula for the mean velocity and wall distance in compressible turbulent wall-bounded flo...
The effect of Reynolds and Mach number variation in compressible isothermal channel flow is investi-...
When analyzing many turbulent flows, the effects of compressibility can be neglected. Even some rela...
This thesis presents the motivation, objectives and reasoning behind the undertaken PhD to investiga...