AN INITIAL STUDY OF THE FLOW AROUND AN AEROFOIL AT HIGH REYNOLDS NUMBERS USING CONTINUATION

摘要: Nonlinearities are an important feature of high Reynolds numbers flows about aircraft. Standard time stepping schemes, used in computational fluid dynamics simulations, unable to capture the whole solution space, breaking down region bifurcations. The extension continuation techniques such is therefore attractive. CFD schemes yield large systems equations and associated difficulties applying methods need be overcome. Whilst previous studies fluids using have been published, these mainly limited much lower numbers. In number flows, inertial forces dominate turbulence must modeled. This study has shown that can effectively for demonstrated through presentation a test cases.