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.
Evaluation of Advanced Two-Phase Flow and Combustion Models for Predicting Low Emission Combustors
Contributed by the International Gas Turbine Institute (IGTI) of THE AMERICAN SOCIETY OF MECHANICAL ENGINEERS for publication in the ASME JOURNAL OF ENGINEERING FOR GAS TURBINES AND POWER. Paper presented at the International Gas Turbine and Aeroengine Congress and Exhibition, Munich, Germany, May 8–11, 2000; Paper 00-GT-133. Manuscript received by IGTI Oct. 1999; final revision received by ASME Headquarters Oct. 2000. Associate Editor: D. Wisler.
- Views Icon Views
- Share Icon Share
- Cite Icon Cite
- Search Site
Klose, G., Schmehl , R., Meier , R., Maier , G., Koch , R., Wittig, S., Hettel , M., Leuckel , W., and Zarzalis, N. (October 1, 2000). "Evaluation of Advanced Two-Phase Flow and Combustion Models for Predicting Low Emission Combustors ." ASME. J. Eng. Gas Turbines Power. October 2001; 123(4): 817–823. https://doi.org/10.1115/1.1377010
Download citation file:
- Ris (Zotero)
- Reference Manager