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
  Synonym:wale

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。
• 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。
• 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
• 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。
• 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 Investigation on Properties of Strake Vortices Using Particle Image Velocimetry
  用粒子图像测速法研究边条涡的性质
• Lateral-Direction Aerodynamic Characteristics and Forebody Strake Control of an Aircraft Undergoing Pitching Oscillation on High Attack Angle
  飞机大迎角俯仰运动下的横侧向气动特性及被动控制
• 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。
• 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。
• 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%。