Open Access
表3
不同构型下变体飞机参数
| τ/(°) | 0 | 5 | 10 | 15 | 20 |
| b/m | 3.347 | 3.344 | 3.318 | 3.269 | 3.195 |
| Sw/m2 | 1.6 | 1.532 | 1.463 | 1.391 | 1.317 |
| cA/m | 0.486 | 0.467 | 0.451 | 0.437 | 0.425 |
| xcg/m | 0.147 | 0.197 | 0.252 | 0.307 | 0.36 |
| Iy/(kg·m-1) | 6.490 | 6.592 | 6.765 | 6.998 | 7.275 |
| τ/(°) | 25° | 30° | 35° | 40° | 45° |
| b/m | 3.099 | 2.981 | 2.841 | 2.681 | 2.503 |
| Sw/m2 | 1.243 | 1.168 | 1.095 | 1.025 | 0.958 |
| cA/m | 0.416 | 0.411 | 0.408 | 0.411 | 0.418 |
| xcg/m | 0.41 | 0.456 | 0.497 | 0.516 | 0.539 |
| Iy/(kg·m-1) | 7.576 | 7.882 | 8.168 | 8.415 | 8.606 |
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