Experimental study of industrial gas turbine flames including quantification of pressure influence on flow field, fuel/air premixing and flame shape

U Stopper, W Meier, R Sadanandan, M Stöhr… - Combustion and …, 2013 - Elsevier
A commercial swirl burner for industrial gas turbine combustors was equipped with an
optically accessible combustion chamber and installed in a high-pressure test-rig. Several …

Numerical prediction of the Flame Describing Function and thermoacoustic limit cycle for a pressurised gas turbine combustor

Y Xia, D Laera, WP Jones… - Combustion Science and …, 2019 - Taylor & Francis
The forced flame responses in a pressurized gas turbine combustor are predicted using
numerical reacting flow simulations. Two incompressible1 large eddy simulation solvers are …

Investigation of an industrial gas turbine combustor and pollutant formation using LES

G Mallouppas, G Goldin… - … Expo: Power for …, 2017 - asmedigitalcollection.asme.org
An experimental variant of a commercial swirl burner for industrial gas turbine combustors
operating at 3 bar is numerically investigated using high-fidelity Computational Fluid …

Investigation of adaptive mesh refinement on an industrial gas turbine combustor

L McManus, M Karalus… - … of Engineering for …, 2023 - asmedigitalcollection.asme.org
An adaptive mesh refinement (AMR) method is demonstrated for Large Eddy Simulations
(LES) of an industrial gas turbine combustor, the SGT-100 provided by Siemens Energy …

[PDF][PDF] Prediction of thermoacoustic instability in gas turbine combustors

Y Xia - 2019 - academia.edu
This thesis numerically predicts thermoacoustic instability in two typical gas turbine
combustors. Incompressible large eddy simulation (LES) is used as the main numerical tool …

Investigation of flamelet generated manifold reaction source term closure models applied to an industrial gas turbine

G Mallouppas, G Goldin… - … Expo: Power for …, 2019 - asmedigitalcollection.asme.org
Abstract Three Flamelet Generated Manifold reaction source term closure options and two
different reactor types are examined with Large Eddy Simulation of an industrial gas turbine …

[PDF][PDF] Dispersion of entropy waves advecting through combustor chambers

Y Xia, I Duran, AS Morgans, X Han - Proceedings of the 23rd …, 2016 - academia.edu
In gas turbines, unsteady combustion generates temperature fluctuations, which are often
termed entropy waves. When these are accelerated through the turbine stages, they …

[图书][B] A numerical method for the prediction of combustion instabilities

D Fredrich - 2020 - researchgate.net
This thesis describes one of the first computational works to investigate the physical
feedback mechanisms associated with self-excited, combustion-driven instabilities in gas …

Modelling of methane and hydrogen enriched methane flames in industrial gas turbine burners

D Moëll - 2018 - portal.research.lu.se
The majority of the power production in the world today is based on combustion of coal, oil
and natural gas. Most countries have agreed that the amount of CO2 emitted to the …

Validation of chemistry acceleration techniques with an industrial gas turbine

G Mallouppas, G Goldin… - … Expo: Power for …, 2019 - asmedigitalcollection.asme.org
Two different numerical techniques for chemistry acceleration are examined with Large
Eddy Simulation of a commercial swirl industrial gas turbine combustor operating at 3 bar …