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.
| Original language | English |
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| Title of host publication | Coal, Biomass and Alternative Fuels; Combustion and Fuels; Oil and Gas Applications; Cycle Innovations |
| Publisher | ASME |
| Volume | 2 |
| ISBN (Electronic) | 9780791878552, 9780791878552 |
| DOIs | |
| Publication status | Published - 1 Jan 2000 |
| Externally published | Yes |
| Event | ASME Turbo Expo 2000: Power for Land, Sea, and Air, GT 2000 - Munich, Germany Duration: 8 May 2000 → 11 May 2000 |
Conference
| Conference | ASME Turbo Expo 2000: Power for Land, Sea, and Air, GT 2000 |
|---|---|
| Country/Territory | Germany |
| City | Munich |
| Period | 8/05/00 → 11/05/00 |