| 1. | Stuffed chicken wings with shrimp paste
香荽鸭翼 |
| 2. | Duck s wing and bear s paw stewed
鸭翼煨熊掌 |
| 3. | 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。 |
| 4. | 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。 |
| 5. | An upper canard , which is in the vicinity height of forward - swept main wing , could improve the maximum lift - to - drag ratio
高于主机翼的鸭翼对最大升阻比的改善较多，但也不宜过高。 |
| 6. | Much more increase of maximum lift - to - drag ratio can be obtained with a forward - swept main wing with a small sweepback angle leading edge
主机翼前掠角较小时，鸭翼改善和提高升阻比的效果比较明显。 |
| 7. | The canards permit the maximum take - off weight to be increased by 700 kg for a penalty of fewer than 5 % in level acceleration time and maximum level speed
虽然鸭翼的存在令最大起飞重量增加了七百公斤，但是最大平飞加速时间和最大平飞速度则相对地减少了5 % 。 |
| 8. | 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。 |
| 9. | In addition to a longer nose , aerodynamic modifications feature kfir - style small nose side - strakes to prevent yaw departure at high aoa , a pair of fixed delta canards on the upper parts of the air intakes , dog - tooth outboard leading - edge extensions , and short fences replacing leading - edge slots
除了一个加长的机鼻外，气动布局的修改包括：在机鼻两则装上可以防止在高攻角下脱离偏航的“幼狮”式小边条，一对固定在进气道的三角鸭翼，锯齿型外翼前缘，和代替前缘翼槽的短翼刀。 |
