Incoming standards on NOx emissions are motivating many aero-engines manufacturers to adopt the lean burn combustion concept. However, several technological issues have to be faced in this transition, among which limited availability of air for cooling purpose and thermoacoustics phenomena that should be managed to safely implement this burning mode. In this scenario, standard numerical design tools are not often capable of characterizing such devices. Thus, considering also the difficulties of experimental investigations in a highly pressurized and reactive environment, unsteady scale resolved CFD methods are required to correctly understand the combustor performances. In the last years Large Eddy (LES) and hybrid RANS-LES models such as Scale Adaptive Simulations (SAS) have undergone considerable developments. Such approaches have been already applied for gaseous flames, leading to a strong enhancement in phenomena prediction with respect to standard steady-state simulations. However, huge research efforts are still required when spray flames are considered, since all the numerical models chosen to describe spray dynamics and the related reactive processes can have a strong impact on the accuracy of the whole simulation. In this work a set of scale resolved simulations have been carried out on the DLR Generic Single Sector Combustor spray flame for which measurements both in non-reactive and reactive test conditions are available. Exploiting a two-phase Eulerian-Lagrangian approach combined with a Flamelet Generated Manifold (FGM) combustion model, LES simulations have been performed in order to assess the potential improvements with respect to steady state solutions. Additional comparisons have also been accomplished with SAS calculations based on Eddy Dissipation combustion model (EDM). The comparison with experimental results shows that the chosen unsteady strategies lead to a more physical description of reactive processes with respect to RANS simulations. FGM model showed some limitations in reproducing the partially-premixed nature of the flame, whereas SAS-EDM proved to be a robust modelling strategy within an industrial perspective. A new set of spray boundary conditions for liquid injection is also proposed whose realiability is proved through a detailed comparison against experimental data.
Skip Nav Destination
ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition
June 13–17, 2016
Seoul, South Korea
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-4975-0
PROCEEDINGS PAPER
Assessment of Scale Resolved CFD Methods for the Investigation of Lean Burn Spray Flames
A. Andreini,
A. Andreini
University of Florence, Florence, Italy
Search for other works by this author on:
D. Bertini,
D. Bertini
University of Florence, Florence, Italy
Search for other works by this author on:
L. Mazzei,
L. Mazzei
University of Florence, Florence, Italy
Search for other works by this author on:
S. Puggelli
S. Puggelli
University of Florence, Florence, Italy
Search for other works by this author on:
A. Andreini
University of Florence, Florence, Italy
D. Bertini
University of Florence, Florence, Italy
L. Mazzei
University of Florence, Florence, Italy
S. Puggelli
University of Florence, Florence, Italy
Paper No:
GT2016-57143, V04AT04A057; 15 pages
Published Online:
September 20, 2016
Citation
Andreini, A, Bertini, D, Mazzei, L, & Puggelli, S. "Assessment of Scale Resolved CFD Methods for the Investigation of Lean Burn Spray Flames." Proceedings of the ASME Turbo Expo 2016: Turbomachinery Technical Conference and Exposition. Volume 4A: Combustion, Fuels and Emissions. Seoul, South Korea. June 13–17, 2016. V04AT04A057. ASME. https://doi.org/10.1115/GT2016-57143
Download citation file:
26
Views
Related Proceedings Papers
Related Articles
Assessment of Scale-Resolved Computational Fluid Dynamics Methods for the Investigation of Lean Burn Spray Flames
J. Eng. Gas Turbines Power (February,2017)
A High-Temperature Catalytic Combustor With Starting Burner
J. Eng. Gas Turbines Power (July,2001)
Flamelet Versus Detailed Chemistry Large Eddy Simulation for a Liquid-Fueled Gas Turbine Combustor: A Comparison of Accuracy and Computational Cost
J. Eng. Gas Turbines Power (January,2022)
Related Chapters
Numerical Modeling of N O x Emission in Turbulant Spray Flames Using Thermal and Fuel Models
International Conference on Mechanical and Electrical Technology, 3rd, (ICMET-China 2011), Volumes 1–3
Advances in the Stochastic Modeling of Constitutive Laws at Small and Finite Strains
Advances in Computers and Information in Engineering Research, Volume 2
Modeling Technique of Product Master Model for Aero Engine Multidisciplinary Collaborative Design and Simulation
Proceedings of the 2010 International Conference on Mechanical, Industrial, and Manufacturing Technologies (MIMT 2010)