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

• 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
• 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%。
• 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。
• 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。
• 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。
• 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。
• 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。
• 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。
• 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