A subgrid stabilization technique is developed for solving the two-dimensional incompressible Navier–Stokes equations at high Reynolds numbers. The time marching algorithm is based on a well-established fractional-step pressure-correction projection method. The advection–diffusion step is enriched by an implicit subgrid stabilizing term and by an explicit dissipative shock capturing term. The former is calculated by means of a hierarchical finite element setting, the latter is included to avoid Gibbs’ phenomenon in the boundary layer. Convergence tests on prototypical two-dimensional examples are reported and the method is used to simulate the viscous incompressible flows around the airfoil NACA0012 at zero incidence and Reynolds numbers ranging from 105 to 106.
Subgrid Stabilized Projection Method for 2D Unsteady Flows at High Reynolds Numbers
MARRA, ANDREA;QUARTAPELLE PROCOPIO, LUIGI
2006-01-01
Abstract
A subgrid stabilization technique is developed for solving the two-dimensional incompressible Navier–Stokes equations at high Reynolds numbers. The time marching algorithm is based on a well-established fractional-step pressure-correction projection method. The advection–diffusion step is enriched by an implicit subgrid stabilizing term and by an explicit dissipative shock capturing term. The former is calculated by means of a hierarchical finite element setting, the latter is included to avoid Gibbs’ phenomenon in the boundary layer. Convergence tests on prototypical two-dimensional examples are reported and the method is used to simulate the viscous incompressible flows around the airfoil NACA0012 at zero incidence and Reynolds numbers ranging from 105 to 106.File | Dimensione | Formato | |
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