combustor的例句大全

an evaporator fitted on a model combustor is investigated to provide uniform circumferential gas temperature profile.

本文介绍一种为环形燃烧室提供油蒸汽的蒸发室。

investigation of atomizers effect on soot concentration and flame radiation in a small model gas turbine combustor experimental investigation of spray characteristics of different nozzles

喷嘴特性对燃烧室内烟粒浓度和火焰辐射的影响喷嘴雾化特性实验研究

experimental study of flame extinction characteristics for a gas turbine combustor burning low btu gas investigation of atomizers effect on soot concentration and flame radiation in a small model gas turbine combustor

低热值煤气燃烧稳定性的试验研究喷嘴特性对燃烧室内烟粒浓度和火焰辐射的影响

application of radiant-tube with regenerative combustor on annealing furnace in zincked-plated plank production line

蓄热式辐射管燃烧器在镀锌板退火炉上的应用

study of raising thermal efficiency of 35t/ h fluidized bed combustor with the ash burn-out bed

35T/H洗矸流化床锅炉加装灰渣燃烬冷却床提高热效率的研究

a set of design parameters were given. the simulation results show that the application of mhd control technology to inlet design can effectively regulate combustor incoming flow state, improve specific impulse and extend the operating range of flight mach number.

给出了一组磁控进气道设计参数，仿真结果表明采用磁控进气道技术可以有效地调节燃烧室进口来流状态，提高比冲，拓宽飞行马赫数范围。

a curve coordinate system was used to simulate cold flow in a typical geometry combustor.

采用曲线坐标，对一个典型的燃气轮机燃烧室的冷态流动进行了数值计算，得到的结果定性合理。

the location of the instability zones is dictated by the combustor geometry and the steady-state combustion characteristics.

不稳定性区域的位置取决于燃烧室几何特性和稳定燃烧特性。

fine singular points burn-out characteristic of micro-char particles in the circulating fluidized bed combustor

循环流化床燃烧室内细焦碳颗粒的燃尽特性分析

self-sustained oscillation will appear in gas turbine combustor when unstable combustion couples with acoustic.

在燃气轮机燃烧室中，当不稳定的燃烧过程与声波相互耦合时，就会产生自激的振动。

analysis and application of gas sampling in the direct-connect supersonic combustor testing

直联式超燃实验台超声速燃气取样分析

In this paper, the body-fitted grids of the combustor with the swirl cup are generated by an elliptical grid generation technique.

本文采用偏微分方程法生成贴体网格，在任意曲线坐标系下数值研究两种先进燃烧室火焰筒及其旋流器三维紊流流场。

under the operating state of the same combustor, the optimized axial location of the fuel nozzle changes with the fuel nozzle spray angle.

在相同的燃烧室工作状态，采用不同喷雾锥角的燃油喷嘴，这个最佳位置不同。

a three-dimensional numerical code has been developed to simulate supersonic reacting flows in scramjet combustor. the code employs an implicit, finite volume, lower-upper ( lu), and time-marching method to solve the complete navier-stokes and species equations in a fully coupled and efficient manner.

采用LU隐式方法强耦合求解有限体积法离散的完全N－S方程及组分方程，数值模拟超燃冲压发动机燃烧室内的化学反应流场。

global one-dimensional finite volume euler equations coupled with chemical reactions are implicitly solved to simulate the reacting flowfield of the combustor of scramjet fueled by hydrogen or hydrocarbon.

本文采用隐式格式强耦合求解有限体积法离散的考虑化学反应的广义一维E uler方程，数值模拟氢或碳氢燃料超燃冲压发动机燃烧室的化学反应流场。

experimental investigation of ignition technology in liquid hydrocarbon fueled scramjet combustor

碳氢燃料超燃冲压发动机点火技术试验

the influence of dual-cavity on pilot hydrogen distribution in scramjet combustor

超燃冲压发动机燃烧室中双凹腔对引导氢分布的影响

configuration effect analysis of scramjet combustor based on the integral balanceable method

基于综合平衡法的超燃冲压发动机燃烧室构型影响分析

the scramjet is composed of inlet, isolator, combustor and nozzle.

超燃冲压发动机由进气道、隔离段、燃烧室和尾喷管组成。

the methodology for scramjet combustor performance analysis and evaluation is build up.

提出了超燃冲压发动机燃烧室的性能分析评价方法。