Table 5 \(C_{\textrm{d}}\) and \(C_{\textrm{l}}\) for a NACA 0012 airfoil at \(\alpha =10^{\circ }\) and \(A=30\) for different boundary conditions
From: Some effects of domain size and boundary conditions on the accuracy of airfoil simulations
Boundary condition | \(\varvec{C}_{\textbf{d}}\) | \(\varvec{C}_{\textbf{l}}\) | Time [s] |
|---|---|---|---|
BC-1 | 0.01294 | 1.07273 | 4,895 |
BC-2 | 0.01598 | 1.05473 | 5,035 |
BC-3 | 0.01294 | 1.07273 | 4,928 |
BC-4 | 0.01294 | 1.07273 | 4,935 |