| 1. | Design and characteristics on wing of extreme big aspect ratio
大展弦比夹芯翼大攻角颤振分析 |
| 2. | 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 |
| 3. | 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 |
| 4. | 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 |
| 5. | Effects of leeside vortex isolation on pressure distribution over a high - alpha body of revolution
背风涡隔离对大攻角旋成体表面压力分布的影响 |
| 6. | The increase of drag coefficient is significant at higher angles of attack
鸭翼增大升力的同时也增大了阻力;大攻角时，鸭翼带来的阻力增量较大。 |
| 7. | Within a multistage environment numerical analysis of the 3 - d viscous flow through the turbine cascades at large incidence
考虑动静干涉的多级透平叶栅大攻角流动特性的三维数值分析 |
| 8. | Then s - style high maneuver trajectory with high angles of attack is simulated by given control commands of angle of pitch
进行了俯仰平面s型轨迹机动飞行仿真，仿真结果说明了大攻角飞行的高机动特性。 |
| 9. | Three - dimensional numerical simulation of the flow characteristics at a large incidence of the variable - geometry power turbine of a marine gas turbine
船用燃气轮机变几何动力涡轮大攻角流动特性的三维数值模拟 |
| 10. | Based on these experimental values , the hydrodynamic forces are identified by a general regression neural network ( grnn ) over a wide range of attack angles
利用这些试验值， grnn神经网络方法可以辨识出大攻角范围内的水动力函数。 |
