Contribution to a conference proceedings/Contribution to a book

FZJ-2018-02928

http://join2-wiki.gsi.de/foswiki/pub/Main/Artwork/join2_logo100x88.png Numerical Investigation of Reacting Flows in Gas Turbine Model Combustors

Fiolitakis, A. ; Eberle, C. ; Grader, M.

2018
Forschungszentrum Jülich GmbH, Zentralbibliothek Jülich

Please use a persistent id in citations: http://hdl.handle.net/2128/18508

Abstract: The present work addresses the simulation of generic gas turbine model combustors by means of computational fluid dynamics. Two different combustors are considered: a pressurised aeroengine model combustor and an atmospheric single-nozzle flameless oxidation (FLOX) combustor. The first of these combustors serves as a validation case for soot models. Results of Large-Eddy Simulations of this combustor in conjunction with a finite rate chemistry combustion model and a comprehensive sectional soot model are presented. The second combustor serves as validation test case for a statistical approach for combustion modelling, namely a transported probability density function method. Simulation results obtained with this statistical approach are presented in this work.

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Contributing Institute(s):

1. John von Neumann - Institut für Computing (NIC)

Research Program(s):

1. 899 - ohne Topic (POF3-899) (POF3-899)

Appears in the scientific report 2018

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Database coverage:

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