Multivariate quadrature-based moments methods for turbulent polydisperse gas–liquid systems

A Buffo, M Vanni, DL Marchisio, RO Fox - International Journal of …, 2013 - Elsevier
The Conditional Quadrature Method of Moments (CQMOM) and the Direct Quadrature
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 …

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 …

LES-based Eulerian PDF approach for the simulation of scramjet combustors

H Koo, P Donde, V Raman - Proceedings of the Combustion Institute, 2013 - Elsevier
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 …

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 …

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 …

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 …

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 …

[PDF][PDF] A realizable multivariate quadrature based approach for supersonic combustion modeling in LES

P Donde, H Koo, V Raman - Proceedings of the 7th US Combustion …, 2011 - Citeseer
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 …