Study on Applicability of Turbulent Combustion Model in the Numerical Calculation of Combustor 湍流燃烧模型在燃烧室数值计算中的应用研究
Porous combustor applying in thermophotovoltaic power system 应用于热光伏系统中的多孔介质燃烧器
A new type of two-color flame monitoring system is developed, and real-time, non-disturbed, spatial tests are performed on a partially premixed methane-air combustor of a gas-fired testing furnace. 开发了一种新型的双色法火焰监测分析系统,并在一台燃气试验炉上对部分预混的甲烷-空气燃烧火焰进行了温度场的空间实时无干扰的测定演示。
Design and development test of a heavy-duty gas turbine combustor 重型燃气轮机燃烧室设计与试验研究
Experimental investigations of a principle model of interaction of pulse detonation combustor ( PDC) with turbine were made by using gasoline and air as fuel and oxidizer. 采用汽油和空气作为燃料和氧化剂,进行了脉冲爆震燃烧室(PDC)与涡轮相互作用的原理性模型试验装置的试验。
The air groove can enlarge the flammable limits of combustor, and make the combustor work at a larger excess air coefficient and a less methane flow rate. 空气槽的存在有助于扩展微燃烧器的可燃极限,使燃烧器在更大的空气过量系数和更小的甲烷流量下工作;
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。
In tests of combustor heat loss arises from radiation in measuring tempera-ture with a thermocouple. 我们在进行某一环形燃烧室扇形形试验件的试验研究时,用热电偶测量了燃烧室内的温度分布。
The model of combustion fraction for dense phase in circulating fluidized bed combustor has been built up, based on thermal balance, gas analysis and total gas amount. 建立了基于热平衡法、烟气分析法和烟气量法的循环流化床锅炉燃烧室密相区燃烧份额计算数学模型,并分析比较了各种模型的特点。
In this paper, the high temperature air combustion technology has been applied on radiant-tube, and designed a new regenerative radiant-tube combustor. 论述了应用高温空气燃烧技术的蓄热式辐射管的实验研究工作,重点研究了辐射管沿长度方向的温度分布规律及其影响因素。
Computations are done on flow configurations that resemble the reaction zone in the scramjet combustor flows. 本文通过数值模拟得到了超燃冲压发动机燃烧室化学反应流流场的流动结构。
Either stall or surge may result in combustor blowout. 不管是喘振或者爆音,都将引起燃烧室的熄火。
Investigation of Step Height Effect on Supersonic Combustor Performance Based on Reaction Flow 基于反应流的台阶高度对超音速燃烧室性能影响研究
Comparison of Turbulent Models for Aero-Engine Combustor Numerical Simulation 航空发动机燃烧室数值仿真中湍流模型的比较研究
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。
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 paper analyses the heating efficiency and the combustor how to affect the output of galvanized sheet. 介绍了镀锌工艺及退火炉的作用,着重分析了退火炉的传热效率和烧嘴能力对镀锌产量的影响。
By the use of a cylindrical coordinate system a numerical simulation was conducted of a single tube return flow combustor flow field. 运用圆柱坐标系对单管回流燃烧室流场进行了数值模拟。
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。
Numerical Simulation of Flow and Heat Transfer in Pulse Combustor Tail Pipe 脉动燃烧器尾管流动与传热数值模拟
Analysis of the combustion and flow field characteristics of advanced vortex combustor 燃烧(废气)分析仪先进旋涡燃烧室流动与燃烧特性分析
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。
The distribution of radiative heat flux to the combustor wall has been obtained by. 通过计算,获得了燃烧室壁面的辐射热流分布。
Numerical study on aerodynamic characteristics of RQL new concept combustor RQL新概念燃烧室气动特性的数值研究
Numerical and Experimental Investigation on a Low NOx Emission Combustor for Micro Gas Turbine 低NOx排放微型燃气轮机燃烧室的数值模拟及实验研究
Numerical analysis of combustion performance in an annular combustor with two-stage swirler; 采用密闭爆发器试验手段,对低易损性发射药的燃烧性能进行了研究。
Heat transfer analysis for actively cooled supersonic combustor 带主动冷却的超声速燃烧室传热分析
The stability of the combustor was rated by use of bombs of varying sizes. 用不同装药量的爆炸弹对燃烧室的稳定性进行评定。
The numerical simulation was used to study the effusion holes on the longitudinal wavy liner in the combustor. 对燃烧室内开有发散孔的纵向波纹隔热屏进行了数值模拟。
By changing the speed and direction of the gas and air entering the combustor, the character of the turbulent field in the combustor is changed. 通过改变燃气和空气进入燃烧室的速度和方向,改变燃烧室内的湍流场特性。