Research Article

Calculation of Hinge Moments for a Folding Wing Aircraft Based on High-Order Panel Method

Table 1

Main parameters of the aircraft.

PropertyMass, m (kg)Center of gravity coordinate, xcg (m)Inertia tensor, Iyy (kg m2)
UnfoldedFoldedUnfoldedFolded

Value8232.45, 0.00, 0.002.45, 0.00, 0.2454755649