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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

    • 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。
    • 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。
    • 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
    • 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。
    • 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
    • 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。
    • This paper gives a review on the technical development of spar platform, including the research on dynamic response, mooring system, fatigue and coupled analysis and the design of heave plate and strake configuration.
      本文介绍Spar平台的发展趋势及其关键技术的研究,包括平台动力响应、系泊系统、疲劳分析、耦合分析以及垂荡板和侧板的设计研究。
    • 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%。
    • 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。
    • 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。