Research Article
Calculation of Hinge Moments for a Folding Wing Aircraft Based on High-Order Panel Method
Table 1
Main parameters of the aircraft.
| Property | Mass, m (kg) | Center of gravity coordinate, xcg (m) | Inertia tensor, Iyy (kg m2) | Unfolded | Folded | Unfolded | Folded |
| Value | 823 | 2.45, 0.00, 0.00 | 2.45, 0.00, 0.24 | 5475 | 5649 |
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