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strake

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

    • 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。
    • 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。
    • Application of Forebody Strake Control Technology
      前体边条控制技术应用
    • 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。
    • 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
    • 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%。
    • 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
    • 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
    • Pressure and velocity fields of spatial cross section on an aircraft model with strake wing and double vertical tails were measured using a seven hole probe.
      采用七孔探针对一种边条翼双垂尾布局的飞机模型进行了空间压力场和速度场的测量。