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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

    • 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。
    • 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%。
    • 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
    • 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。
    • 'Divine Strake'-testing for Iran?
      简氏:“神圣列板”-测试为了伊朗?
    • 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。
    • 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。
    • 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
    • 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
    • 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。