English translation for "升阻比"

aerodynamic fineness
lift drag ratio
lift over drag
lift-drag ratio
lift-over-drag ratio
liftdrag

Related Translations:

阻:  动词(阻挡; 阻碍) block; hinder; impede; obstruct 短语和例子劝阻 dissuade sb. from; advise sb. not to; 拦阻 block; hold back; 阻滞 impede; hinder; obstruct; 风雨无阻 stopped by neither wind nor rain

升:  Ⅰ动词1.(由低往高移动) rise; hoist; go up; ascend 短语和例子升帆 hoist a sail; 把旗升到旗杆顶端。 hoist the flag to the top of the pole. 气球缓缓升上天空。 the balloon rose up slowly into the air. 太阳从东方升起。 the sun rises in

阻升系数:  draglift coefficient

阻升比:  drag lift ratiodrag-life ratiodrag-lift ratiodrag-to-lift ratioratio

Example Sentences:

	1.	Our wingspan will fold us up . - l ve figured the l over d max -翼展可以收起来-我已经计算过最大升阻比
	2.	The film resistance parallel - connected between the emitter and the base of power devices can 薄膜电阻的升阻比尺、 。
	3.	Lift - drag of towed vehicle 拖曳体升阻比
	4.	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。
	5.	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。
	6.	Besides , the design of vane is the major project of the uav research , because the vane is the most important part in power transformation of the uav , the quality of this part will directly affect the capacity of the uav . we should manage to enhance the lift resistance ratio in the same situation 此外,本课题着重对无人机的叶片部分进行设计,因为叶片是无人机的动力转化部分,它的好坏直接影响着飞行器的飞行性能,在相同外部条件下,尽可能使其产生比较大的升阻比。
	7.	The characteristics of the method is that it can modify the guidance coefficients automatically according to the errors between the actual trajectory and the standard trajectory , this is the essential of the standard trajectory guidance . it don " t need any pre - knowledge of the coefficients , this simplifies the problem greatly . following that , the method of predicting the falling site of the instant retuning trajectory is studied 这一方法的特点是从反馈增益系数对再入段纵程偏差修正的本质出发，利用实际弹道和标准弹道的偏差，通过调节升阻比增量，不断修正再入段纵程偏差，最终确定反馈增益系数；这一方法的优点是在求解反馈增益系数时，不必依赖先验知识选取初值，使反馈增益系数的确定更为简便。
	8.	The method of wing shape optimization of space shutlle has been developed with penalty function approach in which the objective function is the mass of the wing and the constraints are the hypersonic re - entry flight cross range , lift / drag ratio , and subsonic flight lift / drag ratio , the margin of the longitudial static stability and the magnitude of the horizontal landing speed etc 摘要介绍了在满足高超音速再入横向机动航程，高超音速再入飞行时的升阻比，亚音速进场飞行时的升阻比，纵向静稳定性裕度和水平着陆速度等飞行性能设计要求下，用罚函数法寻求使航天飞机机翼质量为最小的外形优化方法并给出了算例。
	9.	The results show that the frame of the grid fin has the greatest effect on the grid fin drag characteristics , reducing the drag levels and enhancing the lift - drag ratio for grid fin may be obtained by selecting appropriate frame cross - section shape and thickness of grid fin 计算结果显示，格栅翼的几何结构参数对格栅翼的气动力特性影响很大，格栅翼的边框剖面形状和厚度对格栅翼的阻力影响最大，所以选择合适的边框厚度和剖面形状可以有效地减少格栅翼的阻力，提高升阻比。
	10.	Lastly , previous vane are analysed by fluent , we calculate the pressure distribution chart and report chart of each wing form , then alter the torsion angle and the airfoil form of the vane respectively , finally ascertain the influence curve of the torsion angle and the airfoil form of the vane on which act the lift power 最后,通过fluent对设计出的叶片分析,得出其压力分布图和报告图。然后从改变叶片的扭转角度和翼型两个方面分析其对升力和阻力的影响。得出叶片的扭转角和翼型对升阻比的影响曲线,在文章的结尾部分估算了无人机的一些性能参数。

Similar Words：

"升主动脉压" English translation, "升助" English translation, "升爪" English translation, "升子" English translation, "升宗" English translation, "升阻比调节系统" English translation, "升阻力调节" English translation, "升阻系数曲线" English translation, "升左右的法国大酒桶" English translation, "升佐" English translation