Open Access
表3
分布式吊舱机翼和Tang机翼固有频率对比
| 模态 | nr=1(Tang) | nr=2 | nr=3 |
| 一阶法向弯 | 2.277 | 2.205 | 2.119 |
| 二阶法向弯 | 17.893 | 13.507 | 12.058 |
| 三阶法向弯 | 53.805 | 52.042 | 40.591 |
| 一阶弦向弯 | 15.001 | 14.481 | 13.878 |
| 一阶扭转 | 23.079 | 20.216 | 17.902 |
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