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

Table 4

Geometric characteristics for the original and optimized airfoils.

	Maximum thickness	Location of maximum thickness	Maximum camber	Location of maximum camber	Leading edge radius
Original airfoil	0.089	0.274	0.0197	0.491	0.0078
Optimized airfoil	0.089	0.306	0.0168	0.697	0.0035