Unstructured Large Eddy Simulation for Prediction of Noise Issued from Turbulent Jets in Various Configurations

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Unstructured Large-Eddy Simulations of Supersonic Jets (2017, methodology): “By performing numerical experiments on small grids where we can directly compute the eigenvalues of D, as well as using experience gained from many simulations on a large number of different grids [17,18], we have found that c 2 provides sufficient dissipation to stabilize the Charles operators desc”
Confinement effects in shock wave/turbulent boundary layer interactions through wall-modelled large-eddy simulations (2014, background): “The calculation of α is based on the lack of skew-symmetry of the differencing operator (see Khalighi et al. 2011).”