| 1. | The vertical tail is less affected by the remainder of the airplane .
垂尾受飞机其它部分的影响较小。 |
| 2. | The vertical tail size is not set to avoid spiral instability because this mode is not critical .
垂尾的大小不是根据避免螺旋不稳定来确定的。因为这种运动模态不是设计状态。 |
| 3. | Optimal design of vertical tail using genetic - neural network algorithms
神经网络算法优化飞机垂尾 |
| 4. | The wind - tunnel investigation of the characteristics and mechanism of twin - vertical tail buffet of leading - edge extension configuration
边条翼布局双垂尾抖振特性与机理风洞实验研究 |
| 5. | Notice how the wings aren ' t enlarged and the tailfins aren ' t moved back like the artist ' s impression in the first post shows
注意，和上面那个艺术图比较，机翼没有放大，垂尾也没有移近来。 |
| 6. | Double - wing micro air vehicles adopts the aerodynamic shape : no tail , only wings and vertical tail placing in wing
双翼式微型飞行器采用无尾式,且只有机翼,垂尾也置于机翼上的气动布局。 |
| 7. | Meanwhile , the soft of measured load calculation based on strain method and the soft of theory calculating load on vertical tail are programmed by fortran language
采用fortran语言编制了应变法实测载荷回归计算程序，垂尾载荷理论计算程序。 |
| 8. | In the end , using the product development process of aerofoil rib a software platform which supporting dmpa modeling is developed with software visual c + + 6 . 0 and access 2000
以飞机垂尾的产品开发过程为对象，采用用visualc + + 6 . 0和access2000完成了系统的程序设计，开发了基于dmpa的过程建模系统。 |
