strake
英
美
网络 边条翼; 边条; 列板; 板列; 防滑轮爪
第三人称单数：strakes 过去分词：straked 复数：strakes
COCA.33341
英英释义
noun
- thick plank forming a ridge along the side of a wooden ship
双语例句
- With symmetric forebody strakes or single strake and by varying size and mounting location of the strake, the optimum control scheme of asymmetric forces could be found.
通过边条的对称或单侧布局和匹配边条不同的大小与安装位置，可以找到非对称力的最优控制方案。 - An experimental study of the effects of the twin vertical fins position and twist strake wing on a fighter aerodynamic characteristics was performed in the wind tunnel.
针对边条弯扭及改变双立尾展向位置对全机纵横向气动特性的影响进行了试验研究。 - Experiments show that the adaptability of the self-organized fuzzy controller works very well in different work condition, and can realize variable cushioning strake.
实验结果表明，自组织模糊控制器对不同的工况有较强的适应性，并实现了可变的缓冲行程。 - The required control forces and moments can be obtained using strake control techniques.
采用边条控制技术，可获得所需要的控制力与控制力矩。 - Using strake vortex to reduce the distortion of a Y shaped inlet
利用边条涡抑制Y形进气道流场畸变 - This paper gives a review on the technical development of spar platform, including the research on dynamic response, mooring system, fatigue and coupled analysis and the design of heave plate and strake configuration.
本文介绍Spar平台的发展趋势及其关键技术的研究，包括平台动力响应、系泊系统、疲劳分析、耦合分析以及垂荡板和侧板的设计研究。 - The fixed strake and strake flap will also improve the lift-drag characteristics at medium angles-of-attack, the hinged strake and strake flap will raise the stall behavior.
固定边条和边条襟翼还可改善中小迎角的升阻性能，链接边条和边条襟翼则可使失速性能提高。 - Application of Forebody Strake Control Technology
前体边条控制技术应用 - Based on engineering computations, a reliable aerodynamic calculation method which combined with theoretical research, empirical formulas and the experimental curves was established to calculate the aerodynamic forces of some new strake wing layout projectiles and rockets weapons. A program was compiled with the method.
本课题以工程算法为依据，针对部分边条翼布局的新型弹箭武器，在理论研究的基础上结合经验公式和实验曲线确定一种可靠的气动力计算方法，编制了弹箭气动力计算程序。 - Investigation on the Improvement of Stabilities of Combat Aircraft with Strake Wing Configuration
边条机翼布局战斗机稳定性改进研究