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A joint experimental and LES characterization of the liquid fuel spray in a swirl injector

A joint experimental and LES characterization of the liquid fuel spray in a swirl injector
A joint experimental and LES characterization of the liquid fuel spray in a swirl injector
The quality of liquid fuel spray injection determines to a large extent the steady state performance and dynamics of gas turbine and aero-engine combustors. The present investigation is focused on the detailed characterization of the liquid fuel spray in a single sector test rig targeted at aero-engine applications. The liquid fuel (heptane) is injected in a hollow cone spray pattern by a simplex atomizer and the injector comprises a radial swirler. Two features of the droplet distribution that are less commonly found in the technical literature are identified. First, the distributions of mean droplet diameters exhibit non-axisymmetric patterns, a lack of symmetry that is investigated for three types of swirlers differing by their swirl number and/or head loss. Second, it is found that the size-conditioned velocity distributions feature a single wide peak for small droplets and become bimodal for the largest droplets, with a first peak at low velocities, and a second one at higher velocities. The spray behavior analysis is complemented by making use of Large Eddy Simulations with Lagrangian Particle Tracking. Droplet injection is achieved with a model in which the initial size and velocity distributions are specified from experimental data in the atomizer near field. The initial spray interacts with the lateral injector surface and requires a droplet-wall interaction model accounting for the existence of a liquid film. Simulations do not retrieve the lack of rotational symmetry that is found experimentally indicating that this is not linked to the nature of the swirling flow. This is also consistent with further experiments with a different atomizer confirming that this is due to imperfections in the initial atomizer geometry. Another result is that certain swirler designs appear to be more robust to these atomizer imperfections. Simulations accounting for the liquid film yield a bimodal distribution for the droplets’ axial velocity distribution which would not be obtained without this model indicating that it is important to represent the droplet-wall interaction, a feature that is not commonly found in the literature.
0742-4795
Vignat, Guillaume
f808aa32-377e-48a7-bc60-2db7e1767e09
Rajendram Soundararajan, Preethi
27962fcb-d8a8-405a-b137-086815ec8e29
Durox, Daniel
5abd6445-57f2-41a0-b831-983ef4239273
Vie, Aymeric
605e0f77-a32c-407f-9147-dca4ab5408dc
Renaud, Antoine
aedb2589-2a4a-4614-b9fa-1da56f9c7b0d
Candel, Sebastien
c8f272d5-74e9-4fdf-9052-30122eb3a372
Vignat, Guillaume
f808aa32-377e-48a7-bc60-2db7e1767e09
Rajendram Soundararajan, Preethi
27962fcb-d8a8-405a-b137-086815ec8e29
Durox, Daniel
5abd6445-57f2-41a0-b831-983ef4239273
Vie, Aymeric
605e0f77-a32c-407f-9147-dca4ab5408dc
Renaud, Antoine
aedb2589-2a4a-4614-b9fa-1da56f9c7b0d
Candel, Sebastien
c8f272d5-74e9-4fdf-9052-30122eb3a372

Vignat, Guillaume, Rajendram Soundararajan, Preethi, Durox, Daniel, Vie, Aymeric, Renaud, Antoine and Candel, Sebastien (2021) A joint experimental and LES characterization of the liquid fuel spray in a swirl injector. Journal of Engineering for Gas Turbines and Power, 143 (8). (doi:10.1115/GT2020-14935).

Record type: Article

Abstract

The quality of liquid fuel spray injection determines to a large extent the steady state performance and dynamics of gas turbine and aero-engine combustors. The present investigation is focused on the detailed characterization of the liquid fuel spray in a single sector test rig targeted at aero-engine applications. The liquid fuel (heptane) is injected in a hollow cone spray pattern by a simplex atomizer and the injector comprises a radial swirler. Two features of the droplet distribution that are less commonly found in the technical literature are identified. First, the distributions of mean droplet diameters exhibit non-axisymmetric patterns, a lack of symmetry that is investigated for three types of swirlers differing by their swirl number and/or head loss. Second, it is found that the size-conditioned velocity distributions feature a single wide peak for small droplets and become bimodal for the largest droplets, with a first peak at low velocities, and a second one at higher velocities. The spray behavior analysis is complemented by making use of Large Eddy Simulations with Lagrangian Particle Tracking. Droplet injection is achieved with a model in which the initial size and velocity distributions are specified from experimental data in the atomizer near field. The initial spray interacts with the lateral injector surface and requires a droplet-wall interaction model accounting for the existence of a liquid film. Simulations do not retrieve the lack of rotational symmetry that is found experimentally indicating that this is not linked to the nature of the swirling flow. This is also consistent with further experiments with a different atomizer confirming that this is due to imperfections in the initial atomizer geometry. Another result is that certain swirler designs appear to be more robust to these atomizer imperfections. Simulations accounting for the liquid film yield a bimodal distribution for the droplets’ axial velocity distribution which would not be obtained without this model indicating that it is important to represent the droplet-wall interaction, a feature that is not commonly found in the literature.

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e-pub ahead of print date: 11 January 2021

Identifiers

Local EPrints ID: 505797
URI: http://eprints.soton.ac.uk/id/eprint/505797
ISSN: 0742-4795
PURE UUID: 6d165f67-4fa0-4c27-b887-e10ea1949621
ORCID for Preethi Rajendram Soundararajan: ORCID iD orcid.org/0000-0002-4129-0572

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Date deposited: 20 Oct 2025 16:34
Last modified: 21 Oct 2025 02:12

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Contributors

Author: Guillaume Vignat
Author: Preethi Rajendram Soundararajan ORCID iD
Author: Daniel Durox
Author: Aymeric Vie
Author: Antoine Renaud
Author: Sebastien Candel

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