On the interdependence between flame shape and vortex breakdown mode in turbulent swirling reacting flows
This work uses large-eddy simulations to study the transition of a tulip flame stabilised by bubble vortex breakdown (BVB) mode towards a V flame stabilised by a conical vortex breakdown (CVB). The transition is triggered when the equivalence ratio is increased, resulting in a rise in temperature within the central recirculation zone (CRZ). Simultaneously, the pressure inside the CRZ bubble increases, while the average pressure inside the combustion chamber remains constant. This increase in pressure causes the CRZ bubble to open radially and expand, changing the vortex breakdown mode from BVB to CVB, and the flame shape from a tulip shape to a V shape. A criterion for a limit pressure inside the CRZ was then devised based on the radial momentum equation and the balance between centrifugal force and radial pressure gradient, found to control the radial motion of the CRZ. This criterion helped us to understand the main events of the transition, showing that, once the pressure inside the CRZ exceeds the limit given by the criterion, the flow topology changes from a BVB mode to a CVB mode. This transition highlights the differences between a BVB mode and a CVB mode, showing for the first time that there are characteristic pressure and velocity profiles for each mode in their swirling jets and CRZ. Finally, a significant achievement of this work is the identification of a novel mechanism for the controlled transition of vortex breakdown mode, a combustion-driven transition of vortex breakdown mode.
Authors
- Sébastien Ducruix (ORCID: https://orcid.org/0000-0002-3934-9176)
- Aymeric Vié (ORCID: https://orcid.org/0000-0003-3998-0862)
- Leo Cc Mesquita
Institutions
- HESAM Université (FR)
- Rolls-Royce (United Kingdom) (GB)
Publication Details
- Journal
- Journal of Fluid Mechanics
- Published
- 2026-01-05
- DOI
- https://doi.org/10.1017/jfm.2025.10937
- Primary Topic
- Combustion and flame dynamics
- Type
- article
- Field-Weighted Citation Impact
- 0.00