Noise Investigation of a High Subsonic, Moderate Reynolds Number Jet Using a Compressible Large Eddy Simulation

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COMPUTATIONAL PREDICTION OF FLOW-GENERATED SOUND (2006, methodology): “For instance, Bogey et al. (2003) computed the sound field of a Mach 0.9 jet at a Reynolds number of 6.5 × 104 obtained directly from LES and validated their flow and sound statistics with experimental data.”
Computational aeroacoustics: progress on nonlinear problems of sound generation (2004, neutral): “1) (see compilations in [22,23].”
Wave Packets and Turbulent Jet Noise (2013, methodology): “…of flow-acoustic correlation observed in this region in the above studies, as well as other experimental (Morrison & McLaughlin 1979) and numerical (Bogey et al. 2003, Cavalieri et al. 2011a, Freund 2001) studies that also highlight the dynamics near the close of the potential core as an important…”
An analysis of the correlations between the turbulent flow and the sound pressure fields of subsonic jets (2007, background): “It was previously described from results of a first simulation in Bogey et al. (2003), and was connected to the sound waves radiated in the downstream direction.”