The objective of this research was to further the understanding of the fundamental physical mechanisms which control turbulence and entrainment at different levels of compressibility for supersonic shear flows. Very Large Eddy Simulations (VLES) were performed based on the two-dimensional unsteady Euler equations without any empirical coefficients for turbulence modeling. These equations were used to study the spatially evolving mixing characteristics of unforced, planar, confined shear layers formed by two parallel streams of supersonic air that come into contact after passing over a splitter plate. The computations were performed using the conservative Finite Element Method-Flux Corrected Transport (FEM-FCT) scheme with unstructured adapt...
Direct numerical simulations of supersonic mixing layers and jets have been carried out to study the...
Understanding effects of compressibility on the entrainment and mixing properties of supersonic turb...
We study the organization of turbulence in supersonic boundary layers through large-scale direct num...
The objective of this research was to further the understanding of the fundamental physical mechanis...
Large-eddy simulations of a spatially-evolving turbulent mixing layer have been performed. The flow ...
The Large-Eddy Simulation technique of compressible flows and the effect of compressibility on mixin...
A Large-Eddy Simulation (LES) methodology adapted to the resolution of high Reynolds number turbulen...
Large-eddy simulation (LES) of an under-expanded sonic jet injection into a supersonic turbulent cro...
Recently, through the advent of the dynamic subgrid-scale model, Large-Eddy Simulation (LES) has sho...
Turbulent flows are commonly encountered in the natural world and practical applications. Accurate p...
In this work, experiments on planar free shear layers are conducted to obtain a set of benchmark com...
The turbulent mixing layer has been studied extensively in many experimental undertakings. The insta...
AbstractLarge eddy simulation (LES) of spatially evolving turbulent mixing layer is carried out in t...
This thesis concerns numerical calculations of compressible separated flows, with and without shocks...
A complete understanding of the noise generation mechanisms is prerequisite to reducing aircraft jet...
Direct numerical simulations of supersonic mixing layers and jets have been carried out to study the...
Understanding effects of compressibility on the entrainment and mixing properties of supersonic turb...
We study the organization of turbulence in supersonic boundary layers through large-scale direct num...
The objective of this research was to further the understanding of the fundamental physical mechanis...
Large-eddy simulations of a spatially-evolving turbulent mixing layer have been performed. The flow ...
The Large-Eddy Simulation technique of compressible flows and the effect of compressibility on mixin...
A Large-Eddy Simulation (LES) methodology adapted to the resolution of high Reynolds number turbulen...
Large-eddy simulation (LES) of an under-expanded sonic jet injection into a supersonic turbulent cro...
Recently, through the advent of the dynamic subgrid-scale model, Large-Eddy Simulation (LES) has sho...
Turbulent flows are commonly encountered in the natural world and practical applications. Accurate p...
In this work, experiments on planar free shear layers are conducted to obtain a set of benchmark com...
The turbulent mixing layer has been studied extensively in many experimental undertakings. The insta...
AbstractLarge eddy simulation (LES) of spatially evolving turbulent mixing layer is carried out in t...
This thesis concerns numerical calculations of compressible separated flows, with and without shocks...
A complete understanding of the noise generation mechanisms is prerequisite to reducing aircraft jet...
Direct numerical simulations of supersonic mixing layers and jets have been carried out to study the...
Understanding effects of compressibility on the entrainment and mixing properties of supersonic turb...
We study the organization of turbulence in supersonic boundary layers through large-scale direct num...