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
- 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。 - Optimum computation of relative circumferential position of stay vanes to guide vanes of hydraulic turbine A miniature strake attached to the nose tip of the model can be moved to different circumferential position.
水轮机固定导叶与活动导叶周向相对位置的优化计算根据以上观察，在模型头部安装了微型摆振片，该摆振片可以处在不同的周向位置。 - 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 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。 - 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 - 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。 - 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。 - 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 - 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。