Research Article
Calculation of the Hinge Moments of a Folding Wing Aircraft during the Flight-Folding Process
Table 2
Comparison of statically trimmed results.
| Folding angle (deg) | Platform | Angle of attack (deg) | Deflection angle of the ailerons (deg) |
| 0 | ADAMS | 1.87 | -5.15 | NASTRAN | 1.87 | -5.17 |
| 120 | ADAMS | 6.83 | -8.78 | NASTRAN | 6.76 | -8.54 |
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