Numerical investigation of aeroacoustic interaction in the turbulent subsonic fow past an open cavity
The objective of this thesis is to study numerically the aeroacoustics of low Mach number (M inf 0.3) fow with thick turbulent boundary layer past a cavity based on Large Eddy Simulation (LES). Velocity profiles from power law and equilibrium turbulent boundary layer were imposed as inlet conditions...
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| Format: | Others |
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2010
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| Online Access: | http://oatao.univ-toulouse.fr/7198/1/gandhi.pdf |