许多喷气机都有加力燃烧室。
加力燃烧室的使用导致燃料消耗量的增加。
The use of after-burners results in increased fuel consumption.
由于必须使用加力燃烧室，消耗了较多的燃料。
In consequence of having to use after-burners more fuel is consumed.
不得不使用加力燃烧室，结果燃料消耗量增加了。
After - burners have to be used. As a result fuel consumption is heavier.
主要用作加力燃烧室、导向叶片、涡轮叶片、涡轮盘、喷嘴等。
It can be used adding force combustion chamber, guide vane, turbo vane, turbo table and nozzle etc.
由于这种喷气流中含有大量未燃烧的氧气，在喷管中往往安装加力燃烧室。
Owing to the high proportion of unburnt oxygen in this efflux, afterburners are often provided in the jet -pipe.
由于这种喷气流中含有大量未燃烧的氧气，在喷管中往往安装加力燃烧室。
Owing to the high proportion of unburnt oxygen in this efflux, afterburners are often provided in the jet- pipe .
由于这种喷气流中含有大量未燃烧的氧气，在喷管中往往安装加力燃烧室。
Owing to the high proportion of unburnt oxygen in this efflux, afterburners are often provided in the jet-pipe.
本文对装有钝体火焰稳定器的加力燃烧室燃烧效率特性进行了数值分析和实验研究。
This paper presents the combustion efficiency characteristics of an afterburner with bluff-body flame holders investigated with both numerical and experimental methods.
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。
Based on a turbofan engine, the afterburner is replaced with pulse detonation combustor to form a turbofan-pulse detonation hybrid engine.
该模型的建立为预测航空发动机加力燃烧室振荡燃烧特性及控制规律提供了一种理论探索途径。
The model provides theoretical way for the research of the thermoacoustic oscillation in the aero-engine afterburner.
在用SIMPLE方法计算模型加力燃烧室的流场时，发现SIMPLE方法存在不易收敛的问题。
The fluid fields in modelling afterburner are calculated using SIMPLE procedure, it is found difficult to make the calculation convergence.
本产品有优良的高温抗氧化性，高的热强性。用于燃气导管，加力燃烧室尾喷管，航空用摇摆软管，仪表用管等。
This product has excellent high temperature oxidation resistance, high heat resistance. For a gas conduit, afterburner tail pipe, air hose with a swing, instrumentation pipe.
在任意曲线坐标系下对带有横向波纹隔热屏、外冷却通道和尾喷口的涡喷加力燃烧室的三维热态流场进行数值模拟。
The flow field calculation and buckling analysis were conducted for the afterburner with a heat shield, flame stabilizer and jet nozzle.
在任意曲线坐标系下对带有横向波纹隔热屏、外冷却通道和尾喷口的涡喷加力燃烧室的三维热态流场进行数值模拟。
The flow field calculation and buckling analysis were conducted for the afterburner with a heat shield, flame stabilizer and jet nozzle.
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