1.
Research on Numerical Simulation of Two-Phase Reacting Flow Field and Combustion Performance of Annular Combustors;
环形燃烧室两相燃烧流场与燃烧性能数值研究
2.
Numerical investigation of influence of swirler on combustion performance in annular combustors
数值研究涡流器对环形燃烧室燃烧性能的影响
3.
Measurements of the flow fields in a model annular combustor using particle image velocimetry
应用PIV技术测试模型环形燃烧室流场
4.
Acoustic excitation sources, high order modes and cutoff frequencies of noise were discussed for an annular combustion chamber.
论述了燃烧室的声激励源、环形燃烧室内高阶声模态及其截止频率。
5.
Numerical Simulation of Three-Dimensional Flow Field of Annular Combustor for Aero-Derivative Gas Turbine
航改燃气轮机环形燃烧室三维全流场数值模拟
6.
Analysis of inner acoustic field character of annular combustion chamber modal of aero-engine
航空发动机环形燃烧室模型内部声场特性分析
7.
Laboratorial Reasearch and Numerical Simulation of a Gas Turbine Annular Combustor with Dual-stage Swirler;
单头部双旋流器环形燃烧室性能实验研究和数值模拟
8.
Analysis of Aero-Engine Annular Combustion Chamber Flame Tube Vibration Modes and Acoustic Modes
某型航空发动机环形燃烧室火焰筒振动模态与声学模态分析
9.
Design and experimental research on 6 cm-diameters head-swirl micro-combustor
头部旋涡蒸发管式直径6cm环形燃烧室设计和试验
10.
GMDH method study on annular combustor noise total sound level of aircraft engine
航空发动机环形燃烧室噪声总声级的GMDH方法研究
11.
One study used an eight-foot diameter toroidal combustor, burning liquid oxygen and gaseous hydrogen, with four different injectors.
有一项研究采用8英尺直径的环形燃烧室用四种不同的喷注器，推进剂是液氧和气氢。
12.
CO combustion model for circulating fluidized bed combustor
一氧化碳在循环流化床燃烧室中的燃烧模型
13.
combustion efficiency
燃烧效率燃烧室效率
14.
Oil control ring gap to be located 30 degrees to the left of combustion chamber recess.
控油环间隙位于燃烧室凹口的左30 度。
15.
Numerical study of low emissions for twin annular premixing swirler combustor
双环预混旋流低污染燃烧室数值研究
16.
"These high-voltage surges then cause electric sparks in the combustion chambers. The sparks ignite, or set fire to, the air-fuel mixture in the combustion chambers so that it Burns and causes the engine to operate."
高压电脉冲在燃烧室中形成电火花,引燃燃烧室中的可燃混合气,使发动机运转.
17.
After hydrogen injecting,firstly,a combustion flow pattern developed in the combustion chamber with the flow velocity being supersonic on average.
注入氢后,首先在燃烧室内形成平均流速是超声速的燃烧流动。
18.
Improving Combustion of CNG Engine Through Changing Combustion Chamber Shape and Injection Pattern;
燃烧室形状和喷气规律对天然气发动机燃烧的改善