Open Access
表2
不同俯仰控制方案的几何参数
构型(突起物个数) | 离弹翼前缘的距离/mm | 突起物之间的夹角/(°) |
方案1(1) | 15 | —— |
方案2(2) | 8 | 60 |
方案3(4) | 8, 20 | 60, 40 |
方案4(6) | 8, 16, 24 | 60, 40, 20 |
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