Natural frequencies of selected mode shapes of several aircraft measured at IAE, frequencies are in Hz
| Mode shape | Composite | Aluminum alloy | |||||
|---|---|---|---|---|---|---|---|
| Low wing | Low wing | Low wing | Low wing | High wing | Low wing | High wing | |
| Wing first symmetric bending | 8.0 | 8.3 | 10.0 | 7.6 | 11.6 | 12.3 | 14.8 |
| Wing first antisymmetric bending | 18.4 | 17.5 | 18.4 | 16.7 | 19.9 | 32.8 | 30.5 |
| Tail roll | 12.2 | 11.8 | 14.4 | 13.2 | 16.4 | 15.7 | 15.2 |
| Fuselage first vertical bending | 18.7 | 12.5 | 28.5 | 18.7 | 25.1 | – | 20.1 |
| Fuselage first lateral bending | 22.8 | 21.7 | 18.2 | 21.8 | 19.3 | 21.7 | 17.6 |
| Stabilizer first symmetric bending | 30.2 | 29.4 | 28.5 | 27.6 | 25.1 | 38.7 | 41.5 |
| Fin first bending | 28.8 | 21.7 | 33.6 | 29.5 | 24.2 | 28.5 | 45.4 |
| Mode shape | Composite | Aluminum alloy | |||||
|---|---|---|---|---|---|---|---|
| Low wing | Low wing | Low wing | Low wing | High wing | Low wing | High wing | |
| Wing first symmetric bending | 8.0 | 8.3 | 10.0 | 7.6 | 11.6 | 12.3 | 14.8 |
| Wing first antisymmetric bending | 18.4 | 17.5 | 18.4 | 16.7 | 19.9 | 32.8 | 30.5 |
| Tail roll | 12.2 | 11.8 | 14.4 | 13.2 | 16.4 | 15.7 | 15.2 |
| Fuselage first vertical bending | 18.7 | 12.5 | 28.5 | 18.7 | 25.1 | – | 20.1 |
| Fuselage first lateral bending | 22.8 | 21.7 | 18.2 | 21.8 | 19.3 | 21.7 | 17.6 |
| Stabilizer first symmetric bending | 30.2 | 29.4 | 28.5 | 27.6 | 25.1 | 38.7 | 41.5 |
| Fin first bending | 28.8 | 21.7 | 33.6 | 29.5 | 24.2 | 28.5 | 45.4 |
Source(s):
Table created by authors
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