Fig. 2From: Some effects of domain size and boundary conditions on the accuracy of airfoil simulationsGrid convergence study for a NACA 0012 airfoil at \(\alpha =10^{\circ }\), \(A=30\), and BC-1; a \(C_{\textrm{d}}\) vs number of cells, and b \(C_{\textrm{l}}\) vs number of cellsBack to article page