| 1. | The dash line indicates the possibility of a direct input to the control system through an angle-of-attack indicator .
虚线表示，通过攻角指示器，有可能直接输入到控制系统去。 |
| 2. | Design and characteristics on wing of extreme big aspect ratio
大展弦比夹芯翼大攻角颤振分析 |
| 3. | On cause and research strategy of flow asymmetry in high - alpha flows
大攻角流动非对称性成因与对策 |
| 4. | 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。 |
| 5. | Numerical simulation of 3d flow in a turbine cascade at large incidence
透平叶栅大攻角流动特性的三维数值模拟 |
| 6. | Effect of attack angle messurement error on extracting aerodynamic coefficients
攻角误差对拟合气动系数的影响 |
| 7. | The research of high precision automatic density measurement techniques
利用狭缝相机实现弹丸攻角的高精度测量研究 |
| 8. | 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 |
| 9. | Distribution of angles of attack
攻角分布 |
| 10. | Zero incidence wing
零攻角机翼 |
