Abstract
A swirl stabilized flame has been studied numerically using Large Eddy Simulation. The response of the flame to a large swirl number modulation has as been determined. Decreasing the swirl number moderately does not destabilize the flame. Decreasing further the swirl number induces a transition from stabilized to a jet flame with increase in the flame fluctuations. Increasing back the swirl restores the original configuration. However, the re-stabilization has been found to be considerably slower as compared to the burner aerodynamic time scale. Further studies, including identification of some characteristic turbulent structures, have been carried out. Both a helical and an axial mode have been identified. The helical mode arises in the central recirculation zone, whereas the axial mode arises in the outer shear-layer. Both modes are possible sources of thermo-acoustic instabilities.
Original language | English |
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Title of host publication | 43rd AIAA Aerospace Sciences Meeting and Exhibit - Meeting Papers |
Publisher | American Institute of Aeronautics and Astronautics |
Pages | 4929-4940 |
Publication status | Published - 2005 |
Event | 43rd AIAA Aerospace Sciences Meeting and Exhibit - Reno, NV, United States Duration: 2005 Jan 10 → 2005 Jan 13 |
Conference
Conference | 43rd AIAA Aerospace Sciences Meeting and Exhibit |
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Country/Territory | United States |
City | Reno, NV |
Period | 2005/01/10 → 2005/01/13 |
Subject classification (UKÄ)
- Fluid Mechanics and Acoustics
Free keywords
- Swirl modulation
- Swirl number
- Large Eddy simulation (LES)
- Swirling flame