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Multivariate quadrature-based moments methods for turbulent polydisperse gas–liquid systems
The Conditional Quadrature Method of Moments (CQMOM) and the Direct Quadrature
Method of Moments (DQMOM) are compared with Direct Simulation Monte Carlo (DSMC) for …
Method of Moments (DQMOM) are compared with Direct Simulation Monte Carlo (DSMC) for …
Large-eddy simulation of a supersonic inlet-isolator
H Koo, V Raman - AIAA journal, 2012 - arc.aiaa.org
SUPERSONIC combustion ramjet engines are vital for the realization of hypersonic flight.
Scramjets are relatively simple in design compared to conventional low-speed jet engines …
Scramjets are relatively simple in design compared to conventional low-speed jet engines …
Large-eddy/Reynolds-averaged Navier–Stokes simulations of reactive flow in dual-mode scramjet combustor
JA Fulton, JR Edwards, HA Hassan… - Journal of Propulsion …, 2014 - arc.aiaa.org
Numerical simulations of the turbulent reactive flow within a model scramjet combustor
configuration, experimentally mapped at the University of Virginia's Scramjet Combustion …
configuration, experimentally mapped at the University of Virginia's Scramjet Combustion …
LES-based Eulerian PDF approach for the simulation of scramjet combustors
A probability density function (PDF) approach to account for turbulence–chemistry
interaction in the context of large eddy simulation (LES) based simulation of scramjets is …
interaction in the context of large eddy simulation (LES) based simulation of scramjets is …
Large Eddy/Reynolds-Averaged Navier-Stokes Simulations of Scramjet Combustor Flow Fields
J Edwards, A Potturi, J Fulton - 48th AIAA/ASME/SAE/ASEE Joint …, 2012 - arc.aiaa.org
This paper describes the development of a hybrid large-eddy simulation/Reynolds-averaged
Navier-Stokes (LES/RANS) turbulence modeling framework and its application to various …
Navier-Stokes (LES/RANS) turbulence modeling framework and its application to various …
Large-eddy simulations of scramjet engines
H Koo - 2011 - repositories.lib.utexas.edu
Copyright by Heeseok Koo 2011 Page 1 Copyright by Heeseok Koo 2011 Page 2 The
Dissertation Committee for Heeseok Koo certifies that this is the approved version of the following …
Dissertation Committee for Heeseok Koo certifies that this is the approved version of the following …
Design refinement and modeling methods for highly-integrated hypersonic vehicles
SM Torrez - 2012 - search.proquest.com
A method for early-stage design of high-speed airplanes is presented based on analysis of
vehicle performance, including internal flow in the engine and external flows around the …
vehicle performance, including internal flow in the engine and external flows around the …
Multidisciplinary Optimization of the Fuel Consumption of a Dual Mode Scramjet-Ramjet
S Torrez, D Dalle, J Driscoll - 47th AIAA/ASME/SAE/ASEE Joint …, 2011 - arc.aiaa.org
Dual-mode ramjets have design requirements that are distinct from those of other high
speed propulsion systems because they are expected to operate over a wide range of …
speed propulsion systems because they are expected to operate over a wide range of …
[PDF][PDF] A realizable multivariate quadrature based approach for supersonic combustion modeling in LES
Filtered value of the combustion source term in large eddy simulation (LES) can be
accurately estimated using the joint probability density function (PDF) of species mass …
accurately estimated using the joint probability density function (PDF) of species mass …