Fig. 3. Wing translational (ut+) and rotational (
+) non-dimensional velocities (A), lift coefficient CL (B) and drag coefficient CD (C) plotted against non-dimensional time 
. In B, the quasi-steady lift coefficient is also plotted for comparison.
Fig. 3. Wing translational (ut+) and rotational (+) non-dimensional velocities (A), lift coefficient CL (B) and drag coefficient CD (C) plotted against non-dimensional time . In B, the quasi-steady lift coefficient is also plotted for comparison.