压力分布图的英文

• pressure distribution chart
• pressure distribution pattern
• pressure plotting
• pressure profile
• pressure-distribution pattern
• pressureplotting

• "压力"英文翻译    pressure; tension
• "分布"英文翻译    distribute; spread; scatter; ...
• "图"英文翻译    picture; chart; drawing; map
• "压力分布图绘制" 英文翻译 :    pressure plotting; pressureplotting
• "燃烧室进口气压力分布图" 英文翻译 :    combustor inlet-air pressure profile
• "电力分布图" 英文翻译 :    power distribution map
• "推力分布图" 英文翻译 :    thrust profile
• "应力分布图" 英文翻译 :    stress envelope; stress pattern
• "承压力分布" 英文翻译 :    distributor of bearing pressure
• "土压力分布" 英文翻译 :    earth pressure distribution
• "压力分布" 英文翻译 :    distribution of pressure; distributor of pressure; pressure distribution; pressure field structure; pressure profile; pressuredistribution
• "压力分布环" 英文翻译 :    pressure distribution ring; pressure-distribution ring
• "压力分布律" 英文翻译 :    pressure law
• "大气压力分布" 英文翻译 :    barometric-pressure distribution
• "底部压力分布" 英文翻译 :    base-pressure distribution
• "二维压力分布" 英文翻译 :    two-dimensional pressure distribution
• "法向压力分布" 英文翻译 :    normal pressure distribution
• "基础压力分布" 英文翻译 :    pressure distribution of foundation
• "机翼压力分布" 英文翻译 :    wing pressure distribution
• "简单压力分布" 英文翻译 :    simple pressure distribution
• "接触压力分布" 英文翻译 :    distributor of contact pressure
• "孔隙压力分布" 英文翻译 :    pore pressure distribution
• "脉动压力分布" 英文翻译 :    fluctuating pressure distribution
• "实际压力分布" 英文翻译 :    measured pressure distribution
• "尾翼压力分布" 英文翻译 :    tail pressure distribution

• The author takes consider of the aerial condensability . according to newton ’ s second law and gas equation , it is elicited to the gas pressure distributives in the drill pipe
  通过压力分布图可知,截面突变导致压力发生突变,空气流速在该处最低,因此,最小风量采用截面突变处风速计算。
• In the paper , the computational results of all models are obtained , including 3 - d velocity field , 3 - d pressure field , and six aerodynamic coefficients . the results have good agreement with wind tunnel test
  文中得出了客车外围流场的速度矢量图和压力分布图以及六个气动力系数，并将最终结果与风洞试验结果进行了比较，结果吻合较好。
• This paper explored the micro pressure sensor that is used for the measurement of distributed pressure at the surface of smart - skin . firstly , established the surface pressure model according to the aerodynamic properties , defined the optical measurement system that based on intensity modulation principle , discussed the components of this system and theoretical analyzed its measurement theory in detail
  首先，根据空气流动的基本规律给出机翼表面压力分布图，通过对光学式微型压力传感器的理论分析，采用强度调制法测量飞机机翼表面的压力并建立基于此方法的光学测量系统模型，得到了压力与敏感膜片变形以及光电转换输出能量之间的关系。
• Thirdly , geometry modeling of the pump was made and meshes were divided with gimbit , then the flow filed was investigated using flunt , a commercial available cfd code . as result , lots of internal flow filed of outlet of the gear pump was obtained , including velocity magnitude and pressure magnitude
  应用pro / e和gambit软件对机油泵进行几何建模并划分网格,应用fluent软件模拟多种工况下机油泵出口部分的三维湍流流动,得到详尽的三维湍流场的分析结果,包括压力分布图、速度矢量分布图等。
• Lastly , previous vane are analysed by fluent , we calculate the pressure distribution chart and report chart of each wing form , then alter the torsion angle and the airfoil form of the vane respectively , finally ascertain the influence curve of the torsion angle and the airfoil form of the vane on which act the lift power
  最后,通过fluent对设计出的叶片分析,得出其压力分布图和报告图。然后从改变叶片的扭转角度和翼型两个方面分析其对升力和阻力的影响。得出叶片的扭转角和翼型对升阻比的影响曲线,在文章的结尾部分估算了无人机的一些性能参数。

• 压力分布图的日语：あつりょくぶんぷず