Table 1 Geometric characteristics of the baseline wing
From: A Parametric study on the effects of winglet cant angle on wing aerodynamics and aeroacoustics
Characteristic | Inner Wing | Outer Wing |
|---|---|---|
Root airfoil name | b737a-il | b737b-il |
Tip airfoil name | b737b-il | b737c-il |
Root chord [m] | 7.61 | 3.81 |
Tip chord [m] | 3.81 | 1.36 |
Taper ratio | 0.5 | 0.35 |
Half-span [m] | 5.5 | 11.5 |
Dihedral angle [\(^\circ\)] | 9 | 6 |
