Open Access
表 3
马赫数与迎角对双翼气动特性的影响
| 不确定参数 | CL | CD | ||||
| μ | σ | CV/% | μ | σ | CV/% | |
| 马赫数 | 0.119 3 | 0.002 93 | 2.46 | 0.016 61 | 0.004 33 | 2.61 |
| 迎角 | 0.119 0 | 0.004 35 | 3.66 | 0.016 55 | 0.000 32 | 1.93 |
| 确定性条件 | 0.118 8 | 0.016 54 | ||||
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