Many jets have an afterburner.
许多喷气机都有加力燃烧室。
MSI Afterburner hardware monitoring statistics.
微星加力硬件监测统计。
In the F-15 pilots have to hit afterburner and stay there to go supersonic.
在F - 15上，飞行员要保持超音速飞行就不得不打开加力。
When there is antagonistic to the chin with your fingers from the lip side afterburner.
有拮抗时用手指从颏部向唇方加力。
The afterburner system is completely automatic and can be easily shut down when clean products are being fired.
该重烧系统实现了完全自动化，并且当清洁产品烧制完成后，系统易于关闭。
The model provides theoretical way for the research of the thermoacoustic oscillation in the aero-engine afterburner.
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 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。
In the afterburner, the complicated temperature distribution has close relation with the dilution, combustion and flow of the air and gas.
补燃室内复杂的温度分布和空气与燃气的掺混、燃烧及流动状态有密切关系。
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。
The fluid fields in modelling afterburner are calculated using SIMPLE procedure, it is found difficult to make the calculation convergence.
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。
Firstly, briefly introduced X6 aero-engine, then analyzed the constitution and working principle of the main and afterburner fuel regulators in detail.
首先，对X6发动机的整体情况进行概述，并详细分析了发动机主、加力燃油系统的组成及工作原理；
Afterburner systems, designed to operate up to a stoichiometric overall mixture strength , are always fairly close to combustion instability or screech.
要使加力燃烧系统在理论化学组成量的总混合浓度下还在一直工作，这样的设计通常都很接近于不稳定燃烧或振荡燃烧。
The above experimental result is of value for the mechanism and suppression of low frequency combustion oscillation in an afterburner of a turbofan engine.
上述结果对研究低频振荡燃烧机理和抑制技术有一定的参考价值。
This paper presents the combustion efficiency characteristics of an afterburner with bluff-body flame holders investigated with both numerical and experimental methods.
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。
The numerical simulation of turbulent combustion in the afterburner of solid rocket ramjet was performed by applying the probability density function non -premixed mode.
应用概率密度函数非预混模型，对固体火箭冲压发动机补燃室内的湍流燃烧进行了数值模拟。
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.
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。
The F-22 is characterized by a low-observable, highly maneuverable airframe; advanced integrated avionics; and aerodynamic performance allowing supersonic cruise without afterburner.
歼22的特点是低看得见，高机动性机身；先进的综合航空电子系统；与动力表现让超音速巡航无加力。
The intensity of the gas backflow and axial swirl ond the dilution in the afterburner are enhanced by increasing the air-to-fuel ratio, and then the combustion efficiency is improved.
提高空燃比，可增强补燃室中燃气的回流和轴向涡流强度，加大掺混力度，从而提高燃烧效率。
The intensity of the gas backflow and axial swirl ond the dilution in the afterburner are enhanced by increasing the air-to-fuel ratio, and then the combustion efficiency is improved.
提高空燃比，可增强补燃室中燃气的回流和轴向涡流强度，加大掺混力度，从而提高燃烧效率。
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