Open Access
表1
典型设计工况
| 设计状态 | 飞行高度H/km | 马赫数Ma | 升力系数CL |
| 巡航 | 3 | 0.313 | 0.40 |
| 爬升 | 0 | 0.189 | 0.80 |
| 失速 | 0 | 0.091 | CLmax |
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