Open Access
表9
不同数量的突起物构型下全弹的气动力对比(Ma=2.5，α=0°)
| 构型 | 全弹的滚转力矩/(N·m) | 全弹的轴向力(变化量)/N |
| 无突起物 | 0.0 | 140.68 |
| 方案5 | 0.29 | 151.88(11.20) |
| 方案6 | 0.53 | 161.27(20.59) |
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