Evaluation of advanced Two-Phase flow and combustion models for predicting low emission combustors

Conference Paper (2000)
Author(s)

G. Klose (Karlsruhe Institut für Technologie, Inst.fur Thermische Stromungsmach.)

R. Schmehl (Karlsruhe Institut für Technologie)

R. Meier (Karlsruhe Institut für Technologie)

G. Meier (Karlsruhe Institut für Technologie)

R. Koch (Karlsruhe Institut für Technologie)

S. Wittig (Karlsruhe Institut für Technologie)

M. Hettel (Karlsruhe Institut für Technologie)

W. Leuckel (Karlsruhe Institut für Technologie)

N. Zarzalis (Technische Universität München)

Research Group
Wind Energy
DOI related publication
https://doi.org/10.1115/2000-GT-0133
More Info
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Publication Year
2000
Language
English
Research Group
Wind Energy
Volume number
2
Publisher
ASME
ISBN (electronic)
9780791878552
Event
ASME Turbo Expo 2000: Power for Land, Sea, and Air, GT 2000 (2000-05-08 - 2000-05-11), Munich, Germany
Downloads counter
72

Abstract

The development of low emission aero engine combustors strongly depends on the availability of accurate and efficient numerical models. The prediction of the interaction between two-phase flow and chemical combustion is one of the major objectives of the simulation of combustor flows. In this paper, predictions of a swirl stabilized model combustor are compared to experimental data. The computational method is based on an Eulerian two-phase model in conjunction with an Eddy Dissipation (ED) and a presumed-shape-PDF (JPDF) combustion model. The combination of an Eulerian two-phase model with a JPDF combustion model is a novelty. It was found to give good agreement to the experimental data.

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