Large Eddy Simulation of Supersonic Turbulent Flow in Expansion-Compression Corner

Large Eddy Simulation of Supersonic Turbulent Flow in Expansion-Compression Corner PDF Author: Doyle Knight
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Languages : en
Pages : 12

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Book Description
A Large Eddy Simulation (LES) methodology has been developed for supersonic turbulent flows with strong shock boundary layer interaction. Results are presented for an expansion-compression corner at Mach 3 and compared with experimental data.