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叶栅

n.blade row; cascade of blades
网络vane cascade; blading; lattice

叶栅

英-汉网络释义

叶栅

cascade

风机英语术语_百度文库 ... 翼弦 chord 叶栅 cascade 迎角 angle of attack ...

vane cascade

航海及海运专业术语V(1) ... vane capacitor 叶片式可变电容 vane cascade 叶栅 vane compressor 叶片式压缩机 ...

blade row

英文skid row 翻译下谢谢_百度知道 ... binary row 【自】二进制行 blade row 叶栅 card row 卡片(上的一)行孔, 卡片行 ...

cascade of blades

cellular slime mold的意思中文翻译 ... cascade motor 级联电动机组 cascade of blades 叶栅 cascade particle 级联粒子 ...

blading

气机英语_百度文库 ... blade wheel 叶轮 blading 叶栅 blanket type insulation 垫子式保温 ...

lattice

lattice的翻译中文意思-在线英汉词典 ... lattice n.点阵,格构,晶格 lattice n.叶栅,栅格,格子 lattice 点阵；格子，晶[网]格 ...

blade lattice

泵类产品中英文汉英对照表二 ... 叶梢背部切削 Cutting Back of Impeller Vane Tips 叶栅 blade lattice 叶栅 finite cascade ...

cascades

例句：

The whole flow is divided into three different regions, each being subject to a treatment by the basic aerodynamic flow equations .

将叶栅的整个区域分为三个流动区域并应用流体力学中的基本方程式分别进行了处理。

Calculations have shown that the performance is in its best when fixing the tip winglet on the suction-side .

计算结果表明，端导叶在叶片吸力面侧安装时，叶栅性能最佳。

Separated flow can be efficiently controlled by the flow control technique of using co-flow jets.

采用边界层流动控制能够有效抑制扩压叶栅的流动分离。

The exit flow angle of the two slot types has a little decrease with the increase of ejection ratio .

叶栅出口平均气流角随着喷气比的增大呈减小的趋势，但变化范围很小。

The axisymmetric numerical model of the bypass cascade thrust reverser was established .

建立了外涵叶栅反推器的轴对称计算模型；

In this paper , the shape of stator and rotor cascades was improved and the aerodynamic performance before and after improving was analyzed .

本文对动静叶栅分别进行优化改型，并对改型前后叶栅的气动性能进行数值分析。

To solve the problem of the flow in the nozzle cascade with many splitter vanes , this paper adopts the more advanced finite element method .

为了对这种多分流喷咀叶栅进行全流场计算，本文采用了较先进的气动变分有限元方法。

In this paper a new numerical method is developed to calculate the cascade flow-fields with casing treatment equipment .

提出了一种数值计算带有各种结构机匣处理装置叶栅流场方法。

Topology and Vortex Structures of Turbine Cascade with Different Tip Clearances .

在不同叶顶间隙下涡轮叶栅的拓扑与旋涡结构。

secondly , it realized the whole structure of francis turbine blade surface . thirdly , it accomplished the computation of blade incidence.

第三，针对水轮机叶片的特点，完成了各圆柱面叶栅进口安放角的求解算法。

Reducing the maximum thickness of aerofoil can improve the stage profile efficiency .

减小叶栅最大相对厚度可以提高叶型效率。

At the same time, the development of machining technique makes the cascade profile not just a combination of some simple curves .

同时加工技术的发展使得平面叶栅的外形不再局限于简单几何曲线的组合。

A negative bowed blade increases the flow separation and the flow performance is reduced remarkably .

反弯则使得叶栅内分离趋势增加，气动性能明显降低。

multi-slot configurations have greater effect on outlet flow field than one -slot configurations.

开多孔方案对叶栅出口流场的影响要强于单孔方案。

The Mach number at cascade inlet increasing range was larger with the slot width increased .

缝隙宽度的增大使叶栅进口马赫数升高的幅度也越大。

Addition of bladed-disk makes misted cascade flutter boundaries move forward .

此外，计及盘片耦合效应后，失调叶栅的颤振边界前移。

Three dimensional field of a variable geometry linear turbine cascade is simulated by CFD software NUMECA.

使用 CFD 软件 NUMECA 对变几何平面叶栅三维流场进行了数值模拟。

叶栅

叶栅