Implementation and comparison of three isogeometric NavierStokes solvers applied to simulation of flow past a fixed 2D NACA0012 airfoil at high Reynolds number
Comparison of three isogeometric, incompressible NavierStokes solvers. Simulations of flow around a NACA0012 airfoil at Re=3106 R e = 3  10 6 . Lift, drag and pressure coefficients compared to experiments and simulations. Increasing the element order from 1 to 2 generally improves the results. For p=2 p = 2 the Chorin solver is faster than the VMS and coupled formulation solvers.
naca0012 airfoil isogeometric analysis chorin projection method spalartallmaras variational multiscale