vortex n. (pl. vortexes,-ti-ces ) 1.旋涡;旋风;旋卷行云。 2.【物理学】涡旋;【航空】涡流;【动物;动物学】〔V-〕 单肠涡虫的一属。 the vortex of war 战乱。 the vortex of revolution 革命的旋涡。 be drawn into the vortex of 被卷入…的旋涡中。
generator n. 1.产生者,生殖者,创始者。 2.发电机,发生器。 3.【音乐】基础低音。 4.= generatrix. an A.C. generator交流发电机。 a D.C. generator直流发电机。 an electric generator发电机。 a gas generator煤气发生器。 an induction generator感应发电机。 a shunt generator分[并]激发电机。 a steam generator汽锅,蒸汽发生器。 a thermo generator温差电堆,热电堆,热偶电池。 a timing generator定时信号振荡器。
A study on the reinforced heat exchanging caused by delta winglet pair vortex generators 纵向涡强化换热的实验研究
For several vortex generator jets , the spacing of them was an important factor of effect 对于多个射流,间距是影响其对边界层作用范围的一个重要因素。
Experimental investigation of heat transfer enhancement and pressure drop of some wing - type vortex generators 几种翼型涡流发生器强化换热及流阻性能的实验研究
This paper studied the wake improvement by stern fin and vortex generator numerically 本文中利用数值计算讨论使用艉导流翼与涡流导流翼来改善艉迹流特性的可能性。
Numerical study of interactions of vortices generated by vortex generators and their effects on heat transfer enhancement 扁管翅片通道中涡干涉及其对换热性能的影响
The effect of variation of vortex generator height on heat transfer enhancement performance in finned oblate oval tube test core with six vortex generators per tube 每管六涡扁长椭圆管换热板芯涡产生器翼高对强化传热的影响
A computed study was undertaken to determine the effects of minute vortex generator jets on the zero pressure gradient turbulence boundary layer 本文采用数值模拟方法研究了微型空气涡流发生器对零压力梯度湍流边界层的影响。
He is confident that , someday , with his crafts maneuverability and energy - saving vortex generator ( a device that creates lift much like dragonfly wings ) you wont need airplanes anymore 他相信,总有一天,与他船的机动、节能涡发生器(显示器制造电梯很像蜻蜓翅膀)你不用飞机了
In recent decades , vortex generators used in separation control on wing boundary layer have developed rapidly . some new conceptions such as sub boundary layer , micro & intelligent vortex generators are coming up 近十年来,用于飞机机翼附面层分离控制的涡流发生器发展很快,出现了亚附面层、微型和智能化涡流发生器等新概念。
Provide the experimental research scheme to measure and diagnose boundary layer of airfoil . the satisfied results demonstrated that this scheme is correct and efficient . it provides the reliable foundation on analysis of boundary layer characteristics and vortex generators " design 研究结果表明,该方案是正确的,既切实可行、节约了实验经费,又获得了满意的实验结果,为分析附面层特性和涡流发生器的设计提高了可靠依据。