Open Access
表1
Tang机翼结构参数
| 构件 | 参数 | 数值 |
| 机翼 | 半展长R/m | 0.450 8 |
| 弦长c/m | 0.050 8 | |
| 线密度/(kg·m)-1 | 0.235 1 | |
| 弹性轴惯量距/(kg·m) | 0.205 6×10-4 | |
| 弹性轴位置 | 50% c | |
| 重心位置 | 49% c | |
| 面外弯曲刚度/(N·m2) | 0.418 6 | |
| 面内弯曲刚度/(N·m2) | 0.184 4×102 | |
| 扭转刚度/(N·m2) | 0.953 9 | |
| 翼尖配重 | 质量mp/kg | 0.041 7 |
| 重心位置 | 49% c | |
| X轴转动惯量/(kg·m2) | 0.975 3×10-4 | |
| Y轴转动惯量/(kg·m2) | 0.378 3×10-5 | |
| Z轴转动惯量/(kg·m2) | 0.975 3×10-4 |
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