Open Access
表8
不同俯仰控制方案下全弹的气动力对比(Ma=2.5，α=0°)
| 构型 | 全弹的法向力/N | 全弹的俯仰力矩/(N·m) | 全弹的轴向力(变化量)/N |
| 无突起物 | 0.0 | 0.0 | 140.68 |
| 方案1 | -13.48 | -1.76 | 147.55(6.87) |
| 方案2 | -27.32 | -3.29 | 151.84(11.16) |
| 方案3 | -42.05 | -5.13 | 156.18(15.50) |
| 方案4 | -54.17 | -6.68 | 161.82(21.14) |
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