Aerodynamic Design Optimization of Transonic Natural-Laminar-Flow Airfoil at Low Reynolds Number

Table 6

Geometric characteristics for the optimized airfoils.

	Maximum thickness	Location of maximum thickness	Maximum camber	Location of maximum camber	Leading edge radius
Optimization_1	0.089	0.306	0.0168	0.697	0.00351
Optimization_2	0.089	0.304	0.0170	0.696	0.00345