Open Access
表5
突起物的厚度变化对气动力的影响规律
| 构型 | 弹翼上的阻力/N | 弹翼上的侧向力/N | 突起物产生阻力/N |
| 无突起物 | 11.41 | 0.01 | |
| 矩形 | 11.98 | -9.01 | 6.13 |
| 正方形 | 12.02 | -10.09 | 6.14 |
| 圆形 | 11.96 | -8.23 | 5.29 |
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