侧压的英文

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英文翻译
造句

side compression; side pressure; side thrust; lateral pressure
◇侧压力 lateral compression; wall pressure; lateral pressure; 侧压面 side pressure surface

侧 slant; sloping
压 press; push down; hold down; ...
侧压板 side guide; side-push plate
侧压差 lateral pressure difference
侧压的 tasithynic
侧压力 lateral pressure; lateralpre ure; side compression; side pre ure; side pressure; sidepre ure; wall pressure
侧压面 side pressure surface
侧压腿 press leg at side
侧压下 edge milling; edging draught; indirect draught; indirect rolling action; side pressure; side work
侧压仪 lateral pressure apparatus
壁上侧压孔 wall pressure hole
侧压壁凹 thrust recess
侧压测定仪 tiefensondier apparatus
侧压高度 piezometric height
侧压力；横压力 lateral pressure
侧压力曲线 thrust line
侧压力系数 coefficient of confinement pressure; lateral pressure coefficient; lateral-compression coefficient
侧压力效应 side thrust effect
侧压试验 lateral compression test
侧压水头 piezometric head
侧压系数 coefficient of horizontal pressure
侧压下量 edging
侧压中心 center of lateral pressure
侧压褶皱 buckle folding
等侧压的 isotasithynic

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例句与用法

A parametric analysis of the inviscid effects of leading edge sweep , sidewall compression , width - height ratio , cowl position and inflow mach number on spillage is finished . numerical simulations are completed for a series of inlets at various flight height and velocity . the research indicates that the area of spillage window , which is mainly determined by the position of the cowl , significantly influences the spillage characteristic of the scramjet inlet
阐明了侧板后掠的侧压进气道设计参数对构型溢流影响;对不同侧板配置方式的侧压式进气道进行了数值模拟,通过对比分析,发现由唇口板的位置所决定的溢流窗面积的大小对进气道溢流特性的影响显著。
The results showed that the displacement of the surrounding rock of cavern evidently decreases with the increase of in - situ stress side pressure coefficient , as well as the decreasing rate of surrounding rock displacement of cavern with increasing at the condition of < 1 are significant larger than that of > 1 ; when < 1 , the displacements of measured points in cavern increase then decrease with the increasing incident angle of shear wave , while , when > 1 , the displacements decrease then increase with the increasing incident angle of shear wave , and the influence of incident angle on the displacements of measured points tends to decrease with the increasing in - situ stress side pressure coefficient
分析结果表明，地震荷载作用下，硐室位移随地应力侧压系数的增加明显减小，地应力侧压系数< 1时的硐室位移量值随侧压系数的变化幅度明显大于地应力侧压系数> 1时的情况；当侧压系数< 1 ，随剪切波入射角的变化，硐室测量点位移响应先增加后减小；而当侧压系数> 1 ，随剪切波入射角的增加，硐室测点位移先减小后增加，同时随地应力侧压系数的增加有减小的趋势。
In this thesis , hypersonic sidewall compression inlet ' s self - starting characteristics are numerical simulated and tested . with increasing mach number of inflow gradually , the hypersonic sidewall compression inlets can self - start . compared with the hypersonic sidewall compression inlet starting directly , characteristics are different . moving cowl , decreasing interior contraction ratio also can realize the hypersonic sidewall compression inlet ' s self - starting because of separation bubble on sidewall spilling out
其次,在数值模拟结果的基础上,设计了实验模型和装置并在马赫3 . 85的风洞中进行了移动唇口板减小内收缩比实现侧压式进气道自起动的风洞实验,验证了数值模拟的结果。
Based on matlab system , a multi - layer back propagation neural network model was developed , in which the effects of the depth from surface to the tunnel axis , tunnel diameter , groundwater level , as well as the elastic modulus , shear strength , side pressure coefficient and unit weight of soil and the space between excavated wall and lining on the ground subsidence were considered
采用matlab系统开发了一个多层反向传播神经网络模型，考虑了隧道的深度、隧道的直径、地下水位、土的弹性模量、土的剪切强度、土的侧压系数、土的重度和开挖间隙对地表沉降的影响。
The process of rotary stretch bending without lateral compression and with lateral compression is analyzed separately , and the models of the stress distributing in the section and the springback are also presented separately to discuss the relations between pre - stretch force , lateral compression and the amount of springback . numerous experiments had been done on the equipment of ztlw - 8
本文以等边角型材为研究对象，使用解析法分别对无侧压与侧压转台式拉弯成形过程进行研究，建立了成形区截面的应力分布模型和回弹预测模型，从理论上探讨了回弹半径与预拉力、侧压力的关系。
The code calibration is completed by comparing the numerical results with data from two experiments , one of which is test of a 2 - d hypersonic inlet with internal compression and the other a sidewall compression inlet . good agreement of numerical and experimental results proves the possibility and credibility of the numerical method
利用国外文献公布的二维进气道实验结果和本课题组侧压式进气道炮风洞实验获得的实验数据对本文的计算方法进行了校验,证明了本文所采用的方法应用于高超声速进气道计算的可行性和可靠性。
It is no effect on a sidewall compression inlet ' s starting characteristics while a starting sidewall compression inlet is moved cowl to increase interior contraction ratio appropriately . back pressure effect on characteristics of self - starting for hypersonic sidewall compression inlet is tested in mach 3 . 85 wind tunnel . the hypersonic sidewall compression inlet with interior contraction ratio 1 . 24 can self - start . unstart hypersonic sidewall compression inlet caused by high back pressure can self - start by moving cowl to decrease interior contraction ratio
最后,实验研究了反压对侧压式进气道自起动特性的影响,内收缩比1 . 24的侧压式进气道可以实现自起动并且实验验证了由于反压过高而不起动的侧压式进气道,通过移动唇口板以减小内收缩比可以实现侧压式进气道的自起动。