LES of a pressurized sooting aero-engine model burner using a computationally efficient discrete sectional method coupled to tabulated chemistry-Reference-Cited by-同舟云学术

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LES of a pressurized sooting aero-engine model burner using a computationally efficient discrete sectional method coupled to tabulated chemistry

Published:2024-02 Issue: Volume:260 Page:113198
ISSN:0010-2180
Container-title:Combustion and Flame
language:en
Short-container-title:Combustion and Flame

Author:

García-Oliver J.M.,Pastor J.M.^ORCID,Olmeda I.,Kalbhor A.^ORCID,Mira D.,van Oijen J.A.^ORCID

Publisher

Elsevier BV

Subject

General Physics and Astronomy,Energy Engineering and Power Technology,Fuel Technology,General Chemical Engineering,General Chemistry

Reference64 articles.

1. HPC-enabling technologies for high-fidelity combustion simulations;Mira;Proc. Combust. Inst.,2022

2. Large-eddy simulation of turbulent combustion;Pitsch;Annu. Rev. Fluid Mech.,2006

3. Large eddy simulations of gaseous flames in gas turbine combustion chambers;Gicquel;Prog. Energ. Combust.,2012

4. Modelling of soot aerosol dynamics in turbulent flow;Rigopoulos;Flow Turbul Combust.,2019

5. Modeling of fine-particle formation in turbulent flames;Raman;Annu. Rev. Fluid Mech.,2016

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Imaging diagnostics and PIV measurements of flame propagation and flow structure during ignition process in a three-sector RQL combustor;Aerospace Science and Technology;2024-09

2. Analysis of soot formation in a lab-scale Rich-Quench-Lean combustor using LES with tabulated chemistry;Proceedings of the Combustion Institute;2024

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