Numerical Investigations on Unsteady Features of Rounded Trailing Edge Airfoils

Table 4

for Elliptic264 airfoil.

Reynolds’ number	-6°	-4°	-2°	0°	2°	4°	6°	8°	10°
	0.0027	0.0023	0.0246	0.0407	0.0566	0.0629	0.0610	0.0482	0.0293
	0.0022	0.0075	0.0074	0.0276	0.0490	0.0549	0.0485	0.0355	0.0256
	0.0043	0.0117	0.0099	0.0357	0.0432	0.0446	0.0432	0.0329	0.0163