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This paper conducts Delayed Detached Eddy Simulation (DDES) of a 3D transonic wing flutter using a fully coupled fluid/structure interaction (FSI) with high order shock capturing schemes. Unsteady 3D compressible Navier–Stokes equations are solved with a system of 5 decoupled structure modal equations in a fully coupled manner. The low diffusion E-CUSP scheme with a 5th order WENO reconstruction for...
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