Open Access
表1
不同方法计算的菱形翼型气动力系数及其误差
迎角/(°) | 阻力系数 |
升力系数 |
|||||
CFD | 理论 | 误差/% | CFD | 理论 | 误差/% | ||
0 | 0.029 18 | 0.029 10 | 0.27 | 0 | 0 | ||
2 | 0.032 97 | 0.032 64 | 1.01 | 0.103 5 | 0.101 6 | 1.8 |
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