| 1. | The existence of angle of attack reduces the inlet performance 攻角的存在也在一定程度上降低了进气道性能。 |
| 2. | The velocity distributions previously shown were for a single angle of attack 先前的速度分布列分别为单一迎角 |
| 3. | As seen above , the design angle of attack for the second segment is 10 deg 如上所述,设计攻角的第二部分是10甘醇 |
| 4. | Distribution of angles of attack 攻角分布 |
| 5. | Amplitude in angle of attack 迎角振幅 |
| 6. | Aerodynamic angle of attack 气动迎角 |
| 7. | Angle of attack sensor 迎角传感器 |
| 8. | Critical angle of attack 临界迎角 |
| 9. | Flutter analysis of a high - aspect - ratio sandwich wing under large angle of attack 大展弦比飞机翼身结构不同刚度对结构响应的影响 |
| 10. | Numerical simulation of windward vortex shocks about supersonic slender bodies at high angles of attack 超声速大攻角旋成体迎风激波数值模拟 |