压力面的英文

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"压力面"怎么读用"压力面"造句

英文翻译手机版

acting face
acting surface
pressure face
pressure side
pressure surface

"压力"英文翻译 pressure; tension
"面"英文翻译 face
"反压力面积" 英文翻译 : area of counter pressure
"机翼压力面" 英文翻译 : pressure surface of wing
"桨叶压力面" 英文翻译 : face of propeller blade
"螺桨压力面" 英文翻译 : propeller pressure side
"水翼压力面" 英文翻译 : face of hydrofoil
"压力面积法" 英文翻译 : pressure-area method
"压力面螺距" 英文翻译 : face pitch
"压力面试" 英文翻译 : stress interview
"正压力面" 英文翻译 : normal-pressure surface
"中和压力面" 英文翻译 : neutral pressure plane
"自流压力面" 英文翻译 : artesian pressure surface
"无毛管压力面" 英文翻译 : zero capillary-pressure plane
"压力面推进面" 英文翻译 : acting face
"螺旋桨桨叶压力面" 英文翻译 : face of propeller blade
"就仍然面临着沉重的升值压力面对升值压力" 英文翻译 : rmb/usd
"承力面" 英文翻译 : bearing area; carrying surface
"剪力面" 英文翻译 : plane of shear; shear plane
"升力面" 英文翻译 : carrying piston; lift airfoil; lifting surface; lifting-piston; plane surface; supporting piston; supporting surface
"受力面" 英文翻译 : stress surface; thrust face; thrust surface
"推力面" 英文翻译 : thrust face; thrust surface
"外力面" 英文翻译 : carrying surface
"吸力面" 英文翻译 : suction back; upstream face
"应力面" 英文翻译 : stress plane; stress surface

例句与用法

Acting or driving surface or face
作用面,压力面,推进面螺桨
Propeller pressure side
螺桨压力面
Fire - fighting pumps - fire - fighting centrifugal pumps - requirements for the suction - sided and pressure - sided assembly , test after installation in the fire - fighting vehicle
消防泵.消防离心泵.消防车在安装真空面和压力面组件
Pseudothermal temperature on tension side is higher than that on suction side , and pseudothermal temperature near wall is higher than that in interior
计算结果表明，叶轮吸力面上的颗粒拟温度小于压力面上的，而且靠近壁面处的大于叶道中的。
Time averaged temperature distributions on rotor surface will greatly change with the hot streak / airfoil ratio , and the temperature distribution changes more on the pressure surface than that on the suction surface of the rotor
改变热斑数与导叶通道数比会对动叶时均温度分布产生较大影响，动叶压力面温度分布所受的影响更大。
At the same time , tip leakage induced by pressure gradient and relative motion between the blade tip and the shroud wall is found to have a major influence on detailed flow properties in tip region of rotor passage
同时，由于转子叶片压力面和吸力面之间压力梯度以及叶顶与机匣之问的相对运动产生的间隙流对转子通道内的细微流动结构有较大的影响。
Results show that the influence of mainstream reynolds numbers on heat transfer coefficience is little and the heat transfer coefficience raise with the increase of reynolds numbers . the influence of the position of holes on heat transfer coefficience is complex and correlate with the mainstream speed and the balde surface curvature . and the influence of blowing ratio on heat transfer coefficience is more great ( especially to stator ) , and show a complex relation to mainstream reynolds number and the position of holes
实验结果表明，不同孔位出流的换热由于孔排下游表面来流速度及叶片表面曲率的不同而有不同的规律，而主流雷诺数对叶片表面特别是压力面和前缘区域的换热系数比的影响较小，吹风比对换热系数影响较大(特别是导叶) ，并且随气膜孔位置和来流雷诺数的变化而情况复杂。
Based on an engineering background , through numerical simulation of the flow field in the hp turbine of the energy efficient engine ( e3 ) , the article research the unsteady flow in a transonic turbine stage , the unsteady phenomena in the stage include the shockwave , wake , shedding vortex , endwall vortex , passage vortex and leakage vortex , etc . there are two shockwaves generated on the vane the tailing edge , one on suction side is named moving shockwave , and name another on pressure side steady shockwave
本文首先对于研究的意义和国内外研究的现状做了简要的介绍，再从某工程背景出发，通过对e3发动机高压涡轮内流场的数值模拟，研究了干涉的周期性的问题，以及涡轮级内常见的非定常现象：激波、尾迹、脱落涡、根脚涡、通道涡、漏流涡。导向器尾缘会出现两道激波，在吸力面的激波可称为“运动”激波，压力面的激波可称为“定常”激波。
As we know , inverse techniques make blade ' s profile well compatible with its surface velocity distribution , however , they give designers big challenges that the ideal velocity distribution is hard to obtained and sometimes the non - physical solution , such as double covering of flow field or unclosed profiles , would come out . the proposed design procedure in the paper has avoided the disadvantage mentioned above . in this paper , a quasi - irrotational equation is used to describe the flow in cascade instead of the generally used irrotational equation
众所周知，一般的反问题和混合问题的最大特点，是在给定的压力面和吸力面上的压力分布或速度分布条件下，直接得到叶片的几何形状，它可以使叶型型面与表面气流参数有机结起来；其不足之处在于，对设计者而言，很难给定理想的叶片表面压力分布或速度分布，并且有时会得到一个非物理解，如：得出的初始叶型可能会出现前缘、尾缘不封闭的现象。