Table 9 \(C_\mathrm {d,\infty }\) and \(C_\mathrm {l,\infty }\) for a NACA 0012 airfoil at \(\alpha =5^{\circ }\), \(10^{\circ }\), and \(14^{\circ }\) calculated using the least square extrapolation
From: Some effects of domain size and boundary conditions on the accuracy of airfoil simulations
\(\varvec{C}_{\textbf{d}\varvec{,\infty }}\) | \(\varvec{C}_{\textbf{l}\varvec{,\infty }}\) | |||
|---|---|---|---|---|
\(\varvec{\alpha \,[}^{\varvec{\circ }}\varvec{]}\) | BC-3 | PVBC | BC-3 | PVBC |
5 | 0.00901 | 0.00900 | 0.54916 | 0.54917 |
10 | 0.01216 | 0.01213 | 1.07670 | 1.07676 |
14 | 0.01793 | 0.01791 | 1.45182 | 1.45186 |