来流的英文

• incident flow
• incoming flow
• inflow

• "来"英文翻译    come; arrive
• "来流角" 英文翻译 :    angle of incidence
• "外来流" 英文翻译 :    extraneous current
• "舵来流角" 英文翻译 :    rudder inflow angle
• "来流速度" 英文翻译 :    inflow velocity
• "无忧来流" 英文翻译 :    well upstream
• "相对来流" 英文翻译 :    relative wind
• "近来流行式样" 英文翻译 :    the fashions of yesterday
• "空气来流的扭转" 英文翻译 :    turning of the incoming air
• "来留住你的爱" 英文翻译 :    to make you stay
• "来令片" 英文翻译 :    lining; liquid-vapor separator
• "来龙去脉" 英文翻译 :    sequence of events [actions]; cause and effect; origin and development; the ins and outs; the way(s) and wherefore(s) (of sth.); the entire process; the way it comes and the way it leaves; the whence and whither 我不知道这件事的来龙去脉。 i don't know the ins and outs of the matter
• "来临；流行；插嵌入" 英文翻译 :    set in
• "来鲁华" 英文翻译 :    lai luhua
• "来临，流行" 英文翻译 :    set in
• "来路" 英文翻译 :    1.(向这里来的路) incoming road; approach 六连挡住了敌人的来路。 company six blocked the enemy's path of approach.2.(来源) source
• "来临，来到" 英文翻译 :    advent

• Effect of inlet - air velocity distribution on performance of evaporative condenser
  来流流场对蒸发式冷凝器性能影响的研究
• The simulation results were studied the interaction mechanisms among burning jet flow and upstream flow were demonstrated
  分析和比较了模拟结果，揭示了空气来流和燃气射流对弹箭的干扰机理。
• The equal density and pressure of free streams are chosen to study the effect of compressibility on the mixing layer
  计算选取来流密度和压力相等，对流马赫数从0 . 2到1 . 2 ，以研究压缩性对混合层流动的影响。
• It shows that the model has a good agreement for single - supply alluvial experiment . but the model is n ' t suit for multiple alluvial experiment
  由于缺乏合理的多次堆积模式，对于泥石流多次来流的累加堆积情况不适用。
• The experimental results show that the gridding rib has significant effects on heat transfer enhancement . the nuselts number increases as re increases
  实验结果表明，网格式内冷通道中，随着来流雷诺数re的增加，通道换热效果增强。
• This demonstrates that for propulsion - airframe integration , this genus of inlet would be advantageous in keeping the stability of boundary layer coming from the forebody
  一体化设计时，该进气道对保持前机体来流附面层的稳定性十分有利。
• The flows of pipes in the different conditions with the significant stimulations are solved . the results obtained are analyzed and compared to experimental results referred to
  求解了不同形状管道，不同来流条件下，非微小激励情况下的管内流的流场。
• On basis of this solution , the influence of flow to the vibrating pipe is analyzed and the method of obtaining resonant frequency and resonant time are given
  之后，根据此解，对来流雷诺数的影响进行了分析，并给出了求解、分析共振频率及共振时刻的方法。
• The effect of area ratio , mach number , total pressure of primary rocket and geometry structure of primary rocket on ejectorjet performance was studied
  通过数值计算研究了引射火箭堵塞比、来流马赫数、一次火箭燃烧室总压、一次火箭构型对引射火箭性能的影响。
• The results indicated with the re raising , the rectangle channel ' s heat transfer enhanced gradually , which channel installed the baffle on its above and below
  实验结果表明，上下壁面安装折流板的矩形通道中，随着来流雷诺数re的增加，通道换热效果逐步增强。