这说明了此方法可用于燃烧室性能的分析。
It shows that this method can be applied to the analysis of the combustor feature.
通过本文的研究，空气加湿影响扩散火焰和燃烧室性能的轮廓基本清晰。
After the research work of the present study, the profile of the influence of humid air on diffusion flames and combustor performance becomes basically clear.
结合汽油机燃烧室设计原则对KE495 QME汽油机燃烧室性能进行分析，并对其结构改进设计进行探讨。
This article analyzes the combustion chamber performance of the KE495QME gasoline engine, and discusses how to improve the chamber structure design.
研究了不同进气道和燃烧室结构(六种匹配方案)对燃烧过程和性能的影响。
The effect of different intake port and combustion chamber shape (six modifications in total) on engine combustion and performance were studied.
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 Ground start ignition, altitude restart ignition and combustion stability are important performance indexes to the combustor.
在计算中用一维、定比热容方法分析了相关参数对燃烧室模态转变、性能的影响和隔离段与燃烧室的相互作用。
One dimensional constant specific heat model was taken to analyze the influence of the related parameters on the combustion mode transition and the combustor performance.
提出了超燃冲压发动机燃烧室的性能分析评价方法。
The methodology for scramjet combustor performance analysis and evaluation is build up.
并根据结果分析了燃烧室压强和混合比对发动机性能的影响。
The effects of combustion chamber pressure and mixture ratio on engine performance were analyzed based on simulation.
研究了由推进剂药柱和壳体组成的燃烧室结构径向振动对发动机内弹道性能的影响。
The effect of radial vibration of the chamber structure composed of propellant grain and case on the internal ballistic property of solid rocket motor (SRM) was investigated.
采用遗传算法对某试验超燃冲压模型发动机的燃烧室构型参数进行了优化设计，所得方案的性能大大优于实际方案。
Scramjet combustor design optimization for a test scramjet model engine is conducted by employing genetic algorithms, and an optimal design much better than original design is obtained.
其次通过改变燃烧室构型来研究其对燃烧室内流场和燃烧性能的影响。
The effect of the combustor's shape to the flow and the combustion performance is researched secondly.
研究还发现柔和燃烧具有较高的燃料适应性和变负荷性能，验证了柔和燃烧应用于燃气轮机燃烧室的可行性。
It is found that mild combustion is of wide fuel flexibility and load flexibility, which reflects the feasibility of mild combustion of gas turbine combustor application.
结果表明：喷注汽化燃料有可能改善液体碳氢燃料超声速燃烧室的性能，因为至少省却了雾化和气化过程。
The results suggest that the injection of vaporized fuel would improve the performance of a liquid hydrocarbon-fueled supersonic combustor because the evaporation process is now omitted.
试验表明，使用中心带凸台的缩口型燃烧室后柴油机的性能有所改善。
The test shows that the diesel engine performance can get some improvement when the latter combustion chamber is used.
这些相互冲突的条件要求进行折衷，但是，燃烧室设计与性能的连续改善已经导致燃烧过程“清洁”得多了。
This conflict of conditions requires a compromise to be made, but continuing improvements in combustor design and performance has led to a substantially 'cleaner' combustion process.
根据发动机对燃烧室的性能要求，设计了燃烧室的主要部件，对燃烧室的流量分配及流程参数进行了数值计算。
According to performance requirements of the engine, designed main components of the combustor, calculated flow distribution and flowage parameters of the combustor.
高温升燃烧室头部燃烧组织方案设计，以改善高温升燃烧室的贫油熄火边界及冒烟性能。
A new high temperature rise combustor design with a three-swirler and hybrid injector to improve the smoke emission and lean blow-out characteristics was presented.
在台阶高度一定的条件下，单台阶结构的燃烧室具有更好的燃烧性能。
Furthermore, as the total step height is the same, the combustor configuration with one backwind step has higher performance than the combustor configuration with two backwind step.
本文介绍了由不同几何形状的进气扰动片和燃烧室产生的进气紊流和挤压紊流对直喷式柴油机性能影响的研究。
This paper reports the investigation of the effects of the intake turbulence and the squish turbulence on the performance of a D. I. diesel engine.
地下矿用柴油机的燃烧室型式与其主要性能有密切的关系。本文从废气排放、使用经济性以及噪音等方面对比了两类柴油机的优劣。
The selection of combustion-chamber types of diesel-engines for underground mines is closely related to the performance of the engines themselves.
两种方案对比，在涡轮过渡段设置级间燃烧室空间上更好布置，性能上更占优势。
In general, it is better to set the ITB in turbine transition duct for more sufficient space and more excellent performance improvements.
论述了速燃及新型燃烧室对发动机运行经济性及排放性能的影响，并对新型燃烧室的实验结果进行对比分析，指出了新型燃烧室的特点。
The effects on the operation economical efficiency of the engine and the discharge capability of the new quick burning firebox were discussed in this paper.
用数值解二维N-S动量守恒、能量及组分守恒方程，模拟了一个设置空腔的超燃燃烧室流场参数分布及性能。
The parameter distribution and performance of supersonic combustor with cavity were calculated by means of the solution of 2-D N-S momentum, energy and mass fraction conservation equations.
为直喷式柴油机燃烧室与喷油嘴的合理匹配提供了一条有效途径，对直喷式柴油机性能改进和提高起到重要作用。
It can be a effective way to be offered to optimize the matching of combustion chamber with injection nozzle for direct injection engine. It is of importance to the improvement of...
为直喷式柴油机燃烧室与喷油嘴的合理匹配提供了一条有效途径，对直喷式柴油机性能改进和提高起到重要作用。
It can be a effective way to be offered to optimize the matching of combustion chamber with injection nozzle for direct injection engine. It is of importance to the improvement of...
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