Research Article
Improving Aileron Effectiveness Based on Changing the Position of Aileron Connectors
Table 5
Ten selected modes for flutter.
| Order | Name | Frequency (Hz) | Selected (X) | Reorder |
| 1 | The first rigid mode of the aileron deflection | 1.6E-5 | | | 2 | The first bending mode of the wing | 9.337 | X | 1 | 3 | The first translational mode of the wing | 25.73 | X | 2 | 4 | The flap deflection mode & bending down mode of the aileron | 26.92 | | | 5 | The flap deflection mode & bending up mode of the aileron | 31.056 | X | 3 | 6 | The first bending up mode of the aileron | 40.307 | X | 4 | 7 | The deflection mode of the flap & aileron | 44.25 | X | 5 | 8 | The local mode of the wing | 46.21 | | | 9 | The first torsional mode of the aileron | 60.08 | X | 6 | 10 | The second torsional mode of the aileron | 65.58 | X | 7 | 11 | The translational mode of the flap | 66.27 | X | 8 | 12 | The first torsional mode of the flap | 73.04 | X | 9 | 13 | The first torsional mode of the wing | 75.29 | X | 10 | 14 | The third torsional mode of the aileron | 88.92 | | | 15 | The second torsional mode of the wing | 91.24 | | | 16 | The third torsional mode of the wing | 106.16 | | | 17 | The translational mode of the flap | 112.06 | | | 18 | The fourth torsional mode of the wing | 123.91 | | | 19 | The second bending up mode of the aileron | 126.24 | | | 20 | The local mode of the flap | 129.19 | | |
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