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Time-resolved study of transient soot formation in an aero-engine model combustor at elevated pressure
Abstract The mechanisms of transient formation and oxidation of soot in an aero-engine model combustor at elevated pressure are studied for the first time using a combination of high-speedExpand
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Towards Affordable LES of Rocket Combustion Engines
Due to the large disparity of length and time scales in rocket combustors corresponding LES are highly time consuming. Steps towards simulating rocket combustion engines with affordable LES with theExpand
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Soot model validation by means of LES
Large-Eddy Simulation and Analysis of a Sooting Lifted Turbulent Jet Flame
Abstract A Large-Eddy Simulation (LES) is performed for a sooting, lifted, well characterized, non-premixed, turbulent jet flame. In order to accurately predict the lifted flame, a finite-rateExpand
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Influence of flow field dynamics on soot evolution in an aero-engine model combustor
Abstract Large-Eddy Simulation of a sooting aero-engine model combustor is analyzed by means of proper orthogonal decomposition (POD) to investigate the influence of flow field dynamics on sootExpand