Fig. 10From: Some effects of domain size and boundary conditions on the accuracy of airfoil simulations\({(A^2 \Omega _\mathrm {{I, max}} c)}/{U_{\infty }}\) vs 1/A for a NACA 0012 airfoil at \(\alpha =5^{\circ }\), \(10^{\circ }\), and \(14^{\circ }\) with BC-3Back to article page