| 1. | This induced flow produces a positive moment that increases with wing lift or a .
这一诱导气流产生正的力矩，该力矩随升力或迎角a的增加而增加。 |
| 2. | The conventional tail must be at a negative angle of attack, and the canard tail at a positive angle .
通常的尾翼必须处于负迎角，而鸭式尾翼则为正迎角。 |
| 3. | Curve of moment against incidence
力矩与迎角的关系曲线 |
| 4. | 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 |
| 5. | Anglg - attack transducer sensor
迎角传感器 |
| 6. | Angle - attack transducer sensor
迎角传感器 |
| 7. | Aerodynamic angle of incidence
气动迎角 |
| 8. | Amplitude in angle of attack
迎角振幅 |
| 9. | Aerodynamic angle of attack
气动迎角 |
| 10. | Angle of attack sensor
迎角传感器 |
