Fig. 10From: Adaptive local discontinuous Galerkin methods with semi-implicit time discretizations for the Navier-Stokes equations(a) Adaptive mesh and (b) the contour plots corresponding to P2 solution for subsonic flow around a NACA0012 airfoil, 30 equally spaced contour lines are used to plot Mach number from 0.025 to 0.580Back to article page