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
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。 - 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 - 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。 - 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。 - An experimental study of the effects of the twin vertical fins position and twist strake wing on a fighter aerodynamic characteristics was performed in the wind tunnel.
针对边条弯扭及改变双立尾展向位置对全机纵横向气动特性的影响进行了试验研究。 - 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 - 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 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%。