Implementation of a Fuel Spray Wall Interaction Model in KIVA-II

1991 ◽  
Author(s):  
Leonard K. Shih ◽  
Dennis N. Assanis
Author(s):  
Vignat Guillaume ◽  
Preethi Rajendram Soundararajan ◽  
Daniel Durox ◽  
Aymeric Vié ◽  
Antoine Renaud ◽  
...  

Abstract The quality of liquid fuel spray injection determines to a large extent the performance of aeroengine combustors. The present investigation focuses on the detailed characterization of the liquid fuel spray in a test rig targeted at aeroengine applications. The liquid fuel is injected as a hollow cone by a simplex atomizer and the injector comprises a radial swirler. Two features of the droplet distribution are less commonly found. First, the distributions of droplet diameters exhibit nonaxisymmetric patterns, which are investigated for three types of swirlers. 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 analysis is complemented with Large Eddy Simulations and Lagrangian Particle Tracking. The spray interacts with the lateral injector surface and requires a droplet-wall interaction model for the 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 atomizer geometry. Another result is that certain swirler designs are more robust to atomizer imperfections. Simulations accounting for the liquid film yield a bimodal distribution for the droplets' axial velocity distribution which is not obtained without this model indicating that it is important to represent the droplet-wall interaction.


Author(s):  
Guillaume Vignat ◽  
Preethi Rajendram Soundararajan ◽  
Daniel Durox ◽  
Aymeric Vié ◽  
Antoine Renaud ◽  
...  

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.


2020 ◽  
Vol 30 (3) ◽  
pp. 153-170
Author(s):  
Yaoyu Pan ◽  
Xiufeng Yang ◽  
Song-Charng Kong ◽  
Chol-Bum M. Kweon

Author(s):  
Sheng Meng ◽  
Man Zhang

Abstract This study numerically investigates the effect of spray-wall interactions on thermoacoustic instability prediction. The LES-based flame transfer function (FTF) and the convective time delay methods are used by combining the Helmholtz acoustic solver to predict a single spray flame under the so-called slip and film spray-wall conditions. It is found that considering more realistic film liquid and a wall surface interaction model achieves a more accurate phase lag in both of the time lag evaluations compared to the experimental results. Additionally, the results show that a new time delay exists between the liquid film fluctuation and the unsteady heat release, which explains the larger phase value in the film spray-wall condition than in the slip condition. Moreover, the prediction capability of the FTF framework and the convective time delay methodology in the linear regime are also presented. In general, the instability frequency differences predicted using the FTF framework under the film condition are less than 10 Hz compared with the experimental data. However, an underestimation of the numerical gain value leads to requiring a change in the forcing position and an improvement in the numerical models. Due to the ambiguous definition of the gain value in the convective time delay method, this approach leads to arbitrary and uncertain thermoacoustic instability predictions.


2021 ◽  
Vol 13 (2-3) ◽  
pp. 146-163
Author(s):  
Alejandro Aljure Osorio ◽  
Xavier Tauzia ◽  
Alain Maiboom

Diesel engines are becoming smaller as technology advances, which means that the fuel spray (or jet) interacts with the cylinder walls before combustion starts. Most fuel injection 1D models (especially for diesel fuel) do not consider this interaction. Therefore, a wall-jet sub-model was created on an Eulerian 1D diesel spray model. It was calibrated using data from the literature and validated with experimental data from a fuel spray impacting a plate in a constant volume combustion chamber. Results show that the spray moving along the wall has a higher mixing rate but less penetration as an equivalent free jet, therefore they show a similar volume. Spray-wall interaction creates a stagnation zone right before the impact with the wall, and friction of the jet with the wall is relatively low. All these phenomena are well captured by the wall-jet sub-model.


2000 ◽  
Vol 26 (7) ◽  
pp. 1209-1234 ◽  
Author(s):  
Seong Hyuk Lee ◽  
Hong Sun Ryou

2000 ◽  
Vol 66 (642) ◽  
pp. 604-611 ◽  
Author(s):  
Jiro SENDA ◽  
Tomohiro TAKAHASHI ◽  
Tomoyuki TANAKA ◽  
Ki-Hyung Lee ◽  
Hajime FUJIMOTO

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