1)unstable combustion燃烧不稳
1.The possible of unstable combustion phenomenon of No.分析可能引起2号锅炉燃烧不稳定各种现象的原因,并进行针对性的检查、实验、测量和检修,在运行中采取相应的措施,较好地解决了燃烧不稳的问题。
英文短句/例句
1.combustion instability in rocket engine火箭发动机燃烧不稳定性
2.Combustion instability continues to plague development efforts.燃烧不稳定仍然阻碍研制工作的发展。
3.Premixed Flame Combustion Instability and Its Active Control;预混火焰燃烧不稳定性及其主动控制
4.Experimental study on combustion instability of lean premixed swirl flame贫燃预混旋流火焰燃烧不稳定性的实验
5.Sectored-One-Dimensional Model for Simulating Combustion Instabilities in Premix Combustors一维扇型扫描模型用于模拟预混燃烧室中的燃烧不稳定性
6.There is limited evidence that the mechanism for high frequency combustion instability lies in the vaporization and combustion processes.有限的证据表明，高频燃烧不稳定性机理取决于汽化和燃烧过程。
7.Active control of combustion instability is tested on a cold model.首先，完成了燃烧不稳定性主动控制的冷态实验研究。
8.Analysis of influencing factors of combustion instability in SRM and current progress固体火箭发动机燃烧不稳定的影响因素分析和最新研究进展
9.Experimental method and challenge of the high-frequency combustion instability高频燃烧不稳定性的试验研究方法及面临的挑战
10.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。
11.Flame holders keep a flame going constantly.火焰稳定器维持火焰不断燃烧。
12.To burn unsteadily or fitfully.（火焰）忽明忽暗不稳地或一阵阵地燃烧
13.Numerical Simulation of Combustion Instability of a LOX/GH_2 Rocket Engine氢氧火箭发动机不稳定燃烧数值研究
14.pulsation-free combustion(热风炉)无跳动燃烧， 稳定燃烧
15.Experimental Study on the Thermoacoustic Instability in the Premixed Rijke Combustor;Rijke型预混燃烧器热声不稳定特性的试验研究
16.Experimental Study on Combustion Thermoacoustic Instability under the O_2/CO_2 Atmosphere;O_2/CO_2气氛下的燃烧热声不稳定试验研究
17.Characteristics of Thermoacoustic Instability in a Rijke-type Combustor Under CO_2/O_2 AtmosphereCO_2/O_2气氛下黎开型燃烧器热声不稳定特性
18.At no time can the feed system destabilize an otherwise stable combustion process供应系统决不会使一个在其它状态下稳定的燃烧过程变得不稳定。
相关短句/例句
Unsteady combustion不稳定燃烧
1.To Study the acoustic unsteady combustion of SRM,built the acoustic model of chamber.为研究固体火箭发动机声不稳定燃烧特性,建立了燃烧室内声学特性分析的物理数学模型,推导了小振幅声波三维波动方程,采用有限体积离散方法进行仿真,得到圆柱型、四片翼柱彤和五片翼柱型药柱三种燃烧室形状声学振动基本模态。
2.Analytical results show that the unusual noise source is chiefly due to unsteady combustion.测试结果表明，国产机噪声异常主要是由于不稳定燃烧造成的。
3)combustion instability不稳定燃烧
1.Thermo-acoustic combustion instability in a Solar fuel injector that provides lean premixed combustion conditions was studied with computational fluid dynamics technology.采用CFD方法,可精确地获得燃料到火焰前沿的迟滞时间,证实了所采用的模型能够精确预测不稳定燃烧的出现及振荡特性。
2.The phenomenon of combustion instability is familiar during manufacture the engine in the field of spaceflight, aviation and marine.就发动机燃气发生器发生的不稳定燃烧现象,从声学角度开展了研究,给出了产生不 稳定燃烧的归一化固有频率,进一步设计了声抑制器,并运用有限元分析软件ANSYS对其有效性进行了分析,结 果表明,该声抑制器可以很好的抑制该不稳定燃烧。
4)combustion instability燃烧不稳定
1.A combustion instability detection method that uses the wavelet detail of combustion pressure fluctuations was put forward.针对燃烧不稳定性检测问题,提出利用燃烧压力波动的小波高频分量检测燃烧不稳定性的方法。
2.A preliminary investigation of low frequency combustion instability has been conducted in an atmospheric combustion facility.对模型燃烧室在贫油预混条件下产生的燃烧不稳定性的特性进行了初步研究。
3.According to real time adjusting of propellant flow,based on the variety of combustor pressure,combustion instability is controlled actively.基于压力隐式算子分割(PISO)算法,通过求解Navier-Stokes方程,对煤油/气氧/气氢三组元火箭发动机两相燃烧进行了数值仿真,得到了燃烧自激振荡的仿真结果;根据燃烧室压力变化,通过实时调节推进剂流量,对液体火箭发动机燃烧不稳定进行主动控制。
5)unstable combustion不稳定燃烧
1.An investigation is made to the unstable combustion for combustor,and further for the control purpose a dynamic system and control model is proposed according to the characteristics of the unstable combustion.以发动机不稳定燃烧过程为研究对象,建立起发动机不稳定燃烧力学系统与控制系统的数学模型,进一步应用基于微分几何的反馈线性化方法,将原非线性系统等价为完全可控线性系统,然后设计了滑模控制器。
6)instable combustion不稳定燃烧
1.Finite element method is used in the study of nozzle damping of instable combustion in a solid rocket motor.应用有限单元法研究固体火箭发动机不稳定燃烧中的喷管阻尼，并用波衰减对比法进行了试验研究。
延伸阅读
稳打稳1.形容很有把握。
