| 1. | A variant of the swept-back wing is the delta wing .
后掠翼的变型是三角翼。 |
| 2. | Numerical simulation of internal pressure fields in skew - swept impeller
弯掠翼叶轮内流压力场的计算机数值仿真 |
| 3. | Flow characteristics and its melioration of swept wing body interference
后掠翼身干扰区流动特性及改善措施研究 |
| 4. | Evolution of wave - packet in three - dimensional boundary layer on aswept wing
波包在后掠翼三维边界层中的演化特征 |
| 5. | Numerical simulation of internal secondary vortex in skew - swept impellers
弯掠翼叶轮内流二次涡系的计算机数值仿真 |
| 6. | Variable sweep aerofoil
可变后掠翼 |
| 7. | Backswept wing aircraft
后掠翼飞机 |
| 8. | Variable sweep wing
可变后掠翼 |
| 9. | Canard wing increases lift coefficient with the penalty of the increase of drag coefficient
低于主机翼的鸭翼将加强前掠翼布局的缓失速特性。 |
| 10. | Force measurement in a low speed wind tunnel was conducted to investigate the effects of the height of a distant canard wing on the longitudinal aerodynamic characteristics of a forward - swept configuration
摘要基于前掠翼鸭式前翼布局的风洞测力实验，分析了距离主机翼较远的鸭翼相对于主机翼的高度对布局纵向气动性能的影响。 |
