Open Access
表1
变体飞机不同构型参数
不同后掠角构型/(°) | 机翼参考面积Sw/m2 | 平均气动弦长cA/m | 翼展b/m | 惯性积Ix/ (kg·m2) |
惯性积Iy/ (kg·m2) |
惯性积Iz/ (kg·m2) |
惯性积Ixz/ (kg·m2) |
20 | 0.525 | 0.330 | 1.950 | 3.754 | 6.267 | 4.917 | 0.187 |
50 | 0.525 | 0.330 | 1.544 | 2.662 | 6.307 | 4.865 | 0.185 |
68 | 0.525 | 0.330 | 1.199 | 1.597 | 6.330 | 4.823 | 0.184 |
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