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Large-eddy simulations of turbulent compressible supersonic jet flows using discontinuous Galerkin methods

Communication avec acte
Author
F. ABREU, Diego
471029 Instituto Tecnológico de Aeronáutica = Aeronautics Institute of Technology [Brésil] [ITA]
ccJUNQUEIRA JUNIOR, Carlos
134975 Laboratoire de Dynamique des Fluides [DynFluid]
ccDAURICIO, Eron
471029 Instituto Tecnológico de Aeronáutica = Aeronautics Institute of Technology [Brésil] [ITA]
F. AZEVEDO, João Luiz
471029 Instituto Tecnológico de Aeronáutica = Aeronautics Institute of Technology [Brésil] [ITA]

URI
http://hdl.handle.net/10985/23681
DOI
10.23967/eccomas.2022.162
Date
2022-06

Abstract

In this work, a discontinuous Galerkin scheme is employed to perform the simulations of supersonic jet flows. A total of four simulations are performed with different meshes and order of accuracy. The number of degrees of freedom from the simulations varies from 50 × 10^6 to 400 × 10^6. The results indicate that by increasing the resolution of simulation, in general, the results got closer to experimental data. The jet lipline is the only region in which this behavior is not observed. It investigated a procedure of using lower-order simulations to initialize high-order simulations and consequently reduce the total time of the simulation using high-order schemes. This strategy is successful and allows to perform high-order simulations with only 5% more computational effort than a complete second-order simulation.

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