To reduce emissions in existing combustors, fuel is premixed with a large amount of swirling air flow prior to injection into the combustor.
现行的燃烧室要想减少排放量，必须在燃料注入燃烧室之前就通过大量的空气流将燃料混合好。
Based on a turbofan engine, the afterburner is replaced with pulse detonation combustor to form a turbofan-pulse detonation hybrid engine.
在涡扇发动机基础上，以脉冲爆震燃烧室代替普通加力燃烧室构成涡扇-脉冲爆震组合发动机。
This engine consists of an inlet, a combustor, and a nozzle .
这台发动机由一个进气道，一个燃烧室和一个尾喷管组成。
The annular multi-hole radial jets have important effect on combustor liner.
环向径向射流对燃烧室火焰筒内的流场有着重要的影响。
This paper presents a dump combustor which was designed based on research accomplishment.
文中介绍了一种基于现有研究成果设计的突扩燃烧室。
An annular combustor with evaporation tubes was designed for certain micro-turbojet engine.
为某微型涡喷发动机设计了一个蒸发管环形燃烧室。
Annular reverse flow zone can be found too in the combustor with the flat-straight slag baffle.
简单环形挡渣板也能产生环形回流区，在旋风燃烧室设计中可取代锥形缩口挡渣板。
Micro combustor is one of the most important components of micro thermophotovoltaic (MTPV) system.
微燃烧室是微热光电(MTPV)系统的一个重要组成部分。
The model of combustion efficiency for scramjet combustor is analyzed and presented in this paper.
本文分析及提出了超音速燃烧冲压发动机燃烧室燃烧效率的数学模型。
The present study is concerned with a fluid dynamic research task of interest to the combustor designer.
本文涉及燃烧室设计者感兴趣的流体力学研究课题。
The structure of pulsating combustor which used the technology of thermoacoustic exchange is the simplest.
应用热声转换技术制造的脉动燃烧装置，结构最为简单。
A quasi one dimensional unsteady numerical analysis of supersonic combustor performance has been conducted.
完成了超音速燃烧室内非定常准一维流的数值模拟研究。
The combustion characteristics of an improved Rijke tube pulsating combustor burning diesel oil were studied.
研究了水平安置燃烧柴油的改型瑞克管脉动燃烧器的燃烧特性。
It was found that an increase in the stability of the combustor was obtained simply by gelling the hydrazine.
发现简单地通过肼胶化的方法可使燃烧室的稳定性提高。
SOFC power generation system with chemical looping combustor is a kind of new solid oxide fuel cell combined cycle.
化学链式燃烧器和固体氧化物燃料电池相结合的发电系统是一种新型联合循环。
Measurements were also conducted for the time-averaged gas temperature and species concentrations in the combustor.
同时还测量了该燃烧室内气体平均温度和组分浓度分布。
The performance of supersonic inlet determines the pressure and the air flux in combustor, then affect the work of ramjet.
超声速进气道的性能优劣决定了补燃室流场内的压强和空气流量，进而影响到冲压发动机的工作性能。
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。
These methods have already been used for the gas temperature measurement at the exit of the high temperature rise combustor.
分析和比较了两种计算方法，这些方法已应用到燃烧室出口高温燃气温度测量中。
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。
The PDF method has been applied to investigate the premixed turbulent reactive flows past bluff-body in a rectangle combustor.
本文采用PDF方法对矩形燃烧室内钝体后的湍流预混火焰进行了数值模拟。
The Ground start ignition, altitude restart ignition and combustion stability are important performance indexes to the combustor.
地面起动点火和高空起动点火及燃烧稳定性是燃烧室的重要性能指标。
The three-dimensional flow field of annular combustor for aero-derivative gas turbine burning gas fuel was numerically simulated.
采用数值模拟方法对燃用天然气的某型航改燃气轮机环形燃烧室进行三维流场分析。
The numerical modeling of pulverized coal combustion in an oxygen coal combustor was made by using the continuum trajectory model.
本文采用颗粒相连续介质-轨道模型对同轴射流渐扩式高炉氧煤燃烧器内煤粉燃烧过程进行了数值模拟。
In this paper, the method and some results of cold experimental investigations of liquid slagging coal-fired combustor are described.
本文叙述了液态排渣燃煤燃烧室冷态试验的研究方法和某些结果。
This combustor can be used to billet furnace revolving kiln, forging furnace and other continuously operating industrial furnace and kiln.
该燃烧器可用于轧钢加热炉、回转窑、锻造炉以及其它连续运转的工业炉窑。
Numerical analysis of the kerosene spray supersonic combustion was carried out in the dual-mode supersonic combustor with the CFD software.
利用计算流体力学软件对煤油在所设计的双模态超声速燃烧室内的超声速喷雾燃烧进行了数值模拟。
Turbulent reactive flow in a short annular combustor is simulated by changing the number and location of nozzle and swirler in combustor dome.
通过改变燃烧室头部喷嘴、旋流器的数目和位置，对短环形流燃烧室内有较强回流的湍流旋流流动进行了模拟。
Turbulent reactive flow in a short annular combustor is simulated by changing the number and location of nozzle and swirler in combustor dome.
通过改变燃烧室头部喷嘴、旋流器的数目和位置，对短环形流燃烧室内有较强回流的湍流旋流流动进行了模拟。
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