Chinese translation for "机翼设计"
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- wing design
Related Translations:
机翼特性: wing characteristics 失速机翼: stalled airfoilstalled wing 机翼高度: flügelhhe cushion height 机翼压力系数: wing pressure coefficient 滑翔机的机翼: a glider’s wingsthe wings of a gliderr
- Example Sentences:
| 1. | The joukowski airfoil problem is the simplest application of conformal mapping to airfoil design
Joukowski问题是最简单的翼型形映射应用到机翼设计 | | 2. | In years to come , however , radical wing designs for advanced aircraft may change that
不过在未来几年内，先进飞机所采用的崭新机翼设计可能会改变这一点。 | | 3. | The north wales factory that makes airbus wings is rated as the firm ' s best site , and will retain wing design and final assembly
制造空客机翼的北威尔士工厂被评为该公司最好的厂址，它将继续负责机翼设计和总装配工作。 | | 4. | The integrated aerodynamic / structural design optimization of a simple general aviation aircraft wing demonstrates that the basic two - level optimization is simple in terms of implementation and stable in terms of computation , while the surrogate - based one has the better ability to find the global optimum
轻型飞机机翼设计的算法表明,基本二级优化方法流程简单,稳定可靠;而基于代理模型的二级优化方法全局寻优能力更强。 | | 5. | With the demands of designing the large - scale cargo airplane , in this thesis , many technical materials about the mechanisms of current wing flap types , of foreign transport airplanes are carefully studied at first , and the mechanical composition of three - gaps - fowler - flap is summarized technically about its major basic components , prime mechanism ( track ) , driving device , sub - flaps mechanism and the sub - flaps sequential control system
在本文中，针对大型运输机机翼设计的需求，首先对几种国外运输机襟翼运动机构的资料进行仔细研究，对三缝富勒襟翼运动机构的组成进行了分析，总结归纳出了三缝富勒襟翼运动机构的3个基本组成部分：主机构(轨道) ，驱动机构，子襟翼机构及子襟翼运动控制机构。 | | 6. | Abstract : the effects of airfoil geometric parameters on wing " s spacial and polarized scattering characteristics have been systematically revealed . the results of the study indicated that the calculating value of diffraction from trailing edge by using the formula of the straight wedge is very far from experimental results for vertical polarization , and the contribution of thickness of the trailing edge to scattering must be considered in the calculation . the scattering peak of leading edge depends only on radius of airfoil for horizontal polarization . but for vertical polarization , it depends on maximum thickness and the location of maximum thickness . engineering formulas for evaluating all scattering peaks were given in the paper . it is important for the design of low - rcs wing
文摘:系统地揭示了翼形几何参数对机翼的空间散射特性、极化散射特性的影响规律.研究发现，在垂直极化状态下用理论尖劈公式计算机翼后缘绕射的计算结果与实验结果相差甚远.提出在垂直极化状态下机翼后缘绕射的计算必须将后缘厚度考虑在内的见解.对于水平极化，前缘散射波峰只与前缘半径有关；而对于垂直极化，前缘散射波峰与翼形最大厚度以及最大厚度位置有关.给出前后缘散射波峰的工程估算公式，为低雷达散射截面( rcs )机翼设计提供依据 |
- Similar Words：
- "机翼上的识别标志" Chinese translation, "机翼上反角" Chinese translation, "机翼上方应急出口" Chinese translation, "机翼上翘" Chinese translation, "机翼射击装置" Chinese translation, "机翼设计面积" Chinese translation, "机翼伸展时的翼展" Chinese translation, "机翼升力" Chinese translation, "机翼升力, 翼型升力" Chinese translation, "机翼升力对尾翼绕流的影响" Chinese translation
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