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handle: 2117/192647
The present paper extends the conservative finite element convective scheme proposed by Charnyi et al.(Journal of Computational Physics 337, 2017, 289–308) originally formulated for incompressible flows to the low Mach regime. Similar to Lehmkuhl et al.(Journal of Computational Physics 390, 2019, 51–65) stabilisation is only introduced for the continuity equation by means of a non-incremental fractional-step method, modified in order to account for variable density flows. The final scheme preserves momentum and angular momentum for variable density flows. The error of kinetic energy conservation is of order O(δt hk+1 ), thus dissipation is limited. Standard stabilised finite elements are used for the scalars. Time integration is carried out by means of an explicit third order Runge-Kutta scheme for all equations. The proposed strategy is tested on a set of relevant cases with available reference data using large-eddy simulations. First, an anisothermal turbulent channel flow is assessed. Later, a technically premixed turbulent flame in a swirl-stabilized configuration is considered. And finally, a turbulent jet diffusion flame in a low-velocity co-flow has been studied. In all cases the performance of the presented low Mach formulation is fairly good, showing better accuracy than skew-symmetric like strategies. This project has received funding from the Spanish Ministry of Economy and Competitiveness in the frame of the CHEST project (TRA2017-89139-C2-2-R) and from the European Union’s Horizon 2020 research and innovation programme under the Marie Skłodowska-Curie grant agreement no. 713673. Ambrus Both has received financial support from “la Caixa” Fundation (ID 100010434). The fellowship grant code is LCF/BQ/IN17/11620032. Conflict of Interest: Daniel Mira acknowledges the Juan de la Cierva personal grant IJCI-2015-26686. Peer Reviewed
Elements finits, Finite element method, Kinematics, Reaction effects in flows, Mètode dels, Elements finits, Mètode dels, Combustion, Cinemàtica, :Aeronàutica i espai::Astronàutica::Enginyeria aeroespacial [Àrees temàtiques de la UPC], Low dissipation schemes, Combustió, large-eddy simulation, Finite element, Large-eddy simulation, finite element, low Mach, Àrees temàtiques de la UPC::Aeronàutica i espai::Astronàutica::Enginyeria aeroespacial, Low Mach, low dissipation schemes, Finite element methods applied to problems in fluid mechanics, combustion
Elements finits, Finite element method, Kinematics, Reaction effects in flows, Mètode dels, Elements finits, Mètode dels, Combustion, Cinemàtica, :Aeronàutica i espai::Astronàutica::Enginyeria aeroespacial [Àrees temàtiques de la UPC], Low dissipation schemes, Combustió, large-eddy simulation, Finite element, Large-eddy simulation, finite element, low Mach, Àrees temàtiques de la UPC::Aeronàutica i espai::Astronàutica::Enginyeria aeroespacial, Low Mach, low dissipation schemes, Finite element methods applied to problems in fluid mechanics, combustion
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