Research Article

Shape Optimization of an Airfoil in Ground Effect for Application to WIG Craft

Table 2

Lift to drag ratio (L/D) for original and optimized NACA 4412 airfoil in ground effect for various heights above the ground.

/L/D of original airfoilL/D of airfoil optimized
for / = 0.2
L/D of airfoil optimized
in free stream without ground effect

0.288.3299.9692.56
0.479.0188.1384.50
0.675.2883.8781.21
0.873.3581.7179.50