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
- 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。 - 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。 - 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。 - 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。 - 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。 - 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。 - 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。 - 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。 - 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 - The maximum lift coefficient could be raised by30%. It has been shown that moving surface is an excellent technique to control separated flow over the strake wing.
结果表明，在这种机翼上转动前缘对控制分离是有效的，升力增量最大可达30%。