Data-assisted combustion simulations with dynamic submodel assignment using random forests

WT Chung, AA Mishra, N Perakis, M Ihme - Combustion and Flame, 2021 - Elsevier
This investigation outlines a data-assisted approach that employs random forest classifiers
for local and dynamic submodel assignment in turbulent-combustion simulations. This …

Time-resolved flow field and thermal loads in a single-element GOx/GCH4 rocket combustor

J Zips, C Traxinger, M Pfitzner - International Journal of Heat and Mass …, 2019 - Elsevier
Abstract This work presents Large Eddy Simulations of a single-element GOx-GCH 4
combustion chamber at elevated pressure. A robust and efficient flamelet model accounting …

Large Eddy Simulation of Combustion and Heat Transfer in a Single Element GCH4/GOx Rocket Combustor

D Maestro, B Cuenot, L Selle - Flow, Turbulence and Combustion, 2019 - Springer
The single element GCH 4/GOx rocket combustion chamber developed at the Technische
Universität München has been computed using Large Eddy Simulation. The aim of this work …

A systematic approach to high-fidelity modeling and efficient simulation of supercritical fluid mixing and combustion

X Wang, H Huo, U Unnikrishnan, V Yang - Combustion and Flame, 2018 - Elsevier
Advances in fluid-flow modeling and simulation techniques over the past two decades have
improved understanding of the intricate flow physics and combustion dynamics in the …

Delayed detached eddy simulations with tabulated chemistry for thermal loads predictions

P Breda, M Pfitzner - Journal of Propulsion and Power, 2021 - arc.aiaa.org
The design phase of a rocket combustion chamber relies on the prediction of the wall heat
fluxes, in order to optimize the components to prevent thermal damage. Based on the …

Chemically interconnected light-weight 3D-carbon nanotube solid network

S Ozden, T Tsafack, PS Owuor, Y Li, AS Jalilov… - Carbon, 2017 - Elsevier
Owing to the weak physical interactions such as van der Waals and π-π interactions, which
hold nanotubes together in carbon nanotube (CNT) bulk structures, the tubes can easily …

Efficient time-resolved thermal characterization of single and multi-injector rocket combustion chambers

A Remiddi, G Indelicato, PE Lapenna… - Proceedings of the …, 2023 - Elsevier
In this work, an efficient methodology for the time-resolved thermal characterization of rocket
combustion chambers at reasonable computational cost is presented. The multi-scale and …

[PDF][PDF] Generation of non-adiabatic flamelet manifolds: comparison of two approaches applied on a single-element GCH4/GO2 combustion chamber

P Breda, M Pfitzner, N Perakis, O Haidn - 8th European Conference for …, 2019 - eucass.eu
This work aims to compare two non-adiabatic flamelet combustion models for the simulation
of a subscale single-injector GCH4/GO2 combustion chamber in rocket-like operative …

Reduced kinetic mechanism for methane/oxygen rocket engine applications: a reliable and numerically efficient methodology

G Saccone, P Breda, P Natale… - Combustion Theory and …, 2023 - Taylor & Francis
CFD simulations of turbulent reacting flows based on finite rate chemistry often employ
reduced kinetic mechanisms to decrease the computational cost, especially if the …

[PDF][PDF] Large Eddy Simulation of flow and combustion in a single-element GCH4/GOX rocket combustor

D Maestro, B Cuenot, L Selle - 7th European Conference for …, 2017 - eucass.eu
A single element GCH4/GOx rocket combustion chamber has been computed, via Large
Eddy Simulation of the experimental combustion rig developed at the Technische Universität …