Improved Delayed Detached Eddy Simulation of AGARD Wing Flutter with Fully Coupled Fluid-Structure Interaction

The Shear Stress Transport model based improved delayed detached eddy simulation of the AGARD Wing 445.6 is performed at the subsonic, transonic and supersonic flow with high order shock capturing schemes. An implicit unfactored Gauss-Seidel line iteration scheme is used to solve the compressible, filtered Navier-Stokes equations. The flow solver and the modal form structural solver utilize the dual time-stepping scheme to achieve fully coupled...