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Detached-Eddy Simulation of the Reentry-F Flight Experiment
July 01, 2012
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Evaluation of Wall Modeled Large Eddy Simulation of Cold Wall Hypersonic Boundary Layer
Large eddy simulation (LES) of wall bounded high Reynolds number flows is challenging due to strict cell size and time-step requirements necessary to resolve the inner layer. This restriction motivated the development of wall models which approximate the ...
- Direct Numerical Simulation of Crossflow Instability Excited by Microscale Roughness on HIFiRE-5
- Evaluation of a subgrid-scale model for the temperature fluctuations in reacting turbulence
- Optimization of weighted ENO schemes for DNS of compressible turbulence
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Stability Analysis of HIFiRE 1 with Flight Wall Temperatures
Laminar to turbulent boundary layer transition is sensitive to wall temperature distribution and freestream disturbances. The wall temperature can increase the boundary layer thickness and affect the growth rate of disturbances in the boundary layer. ...
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Turbulent Dissipation-Rate Equation for Compressible Flows
June 01, 2003
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Wall-Modeled Large-Eddy Simulation of Autoignition-Dominated Supersonic Combustion
July 01, 2017
Simulations of combustion in high-speed and supersonic flows need to account for autoignition phenomena, compressibility, and the effects of intense turbulence. In the present work, the evolution-variable manifold framework of Cymbalist and Dimotakis (“On ... - Grid Sensitivity of Detached Eddy Simulation of a Mach 16 Re-Entry Configuration
- DNS of Transition To Turbulence in a Mach 6 Boundary Layer
- Assessment of the k-epsilon turbulence model for compressible flows using direct simulation data
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Computational Verification of Acoustic Damping in High-Enthalpy Environments
November 01, 2014
- DNS of transition to turbulence in a hypersonic boundary layer
- Direct Numerical Simulation of Trip Induced Transition
- Effect of chemical reactions on the decay of isotropic homogeneous turbulence
- Temperature fluctuation scaling in reacting boundary layers
- Filtered Mass Density Function for Variable-Density Turbulent Reactive Flows on Unstructured Meshes
- An implicit essentially nonoscillatory method for the direct simulation of supersonic turbulent boundary layers
- Hybrid RANS/LES Simulation of Injection and Mixing in the CUBRC Combustion Duct
- DNS of a Mach 4 boundary layer with chemical reactions