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。 - 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。 - Some unusual control surfaces such as spoiler, clam-shell aileron, body-nose strake, movable wing-tip are investigated on two typical configurations.
在两种典型布局上研究了扰流板、开裂副翼、机头边条、活动和偏转翼梢及舵面的方向控制特性。 - The valve is driven directly by a large strake multilayer piezoelectric stack, its displacement actuates the power cascade spool after amplification by a lever mechanism.
该阀采用大行程的压电叠堆作为驱动元件，经杠杆放大后的位移直接驱动功率级滑阀。 - 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。 - A Big Cheater Research on the Strake Wing Vortex Lift of Flighter at High Angle of Attack
战斗机边条翼大迎角涡升力研究 - Some measures improving the longitudinal and lateral stabilities of combat aircraft with strake wing configuration are discussed.
对边条机翼布局战斗机的纵、横向稳定性改进措施进行了研究。 - Results indicate that the strength of the strake vortex increases with a quadric function of the attack angle and the type of vortex breakdown is spiral breakdown in this experiment.
实验结果表明边条涡强度随攻角呈平方关系增长，边条涡的破碎形态为单螺旋破碎。 - Combined with the examples of structure, it also makes recommendations for the strake installation. The result can be achieved to reduce VIV of the purpose of fatigue damage and was able to meet the requirements of the fatigue life.
并且结合本文实例，对螺旋导板的安装提出了建议，可以达到减小涡激振动疲劳损伤的目的，又能够满足疲劳寿命的要求。 - Research on the Low Speed Aerodynamic Characteristics of an Aircraft with a Small Strake and Controlling Separation at the Outer Part of Its Wing
一种小边条飞机的低速气动特性及其外翼分离控制研究