supersonic combustion发音

意思翻译

超音速燃烧

相似词语短语

combustion───n.燃烧，氧化；骚动

combustion air───[热]助燃空气；[热]燃烧空气

combustion chamber───燃烧室; 炉膛；[动力]燃烧室

spontaneous combustion───n.自燃

combustion tube───[分化]燃烧管；纵火筒

internal combustion───内燃（烧）

internal combustion engine───[动力]内燃机

combustion and flame───燃烧与火焰

flamelet combustion model───小火焰燃烧模型

双语使用场景

The mixture-fraction equilibrium chemistry model and discrete droplet model can predict correctly kerosene spray supersonic combustion.───混合分数平衡化学反应模型和离散液滴模型能准确地预测煤油在双模态燃烧室内的喷雾燃烧。

The results show that some of technological problems for experimental investigation on supersonic combustion with shock tunnels have been solved basically.───结果表明激波风洞用于超声速燃烧研究的一些必要的技术问题已基本解决。

Numerical analysis of the kerosene spray supersonic combustion was carried out in the dual-mode supersonic combustor with the CFD software.───计算流体力学软件对煤油在所设计的双模态超声速燃烧室内的超声速喷雾燃烧进行了数值模拟。

One answer could come from a supersonic combustion ramjet, known as a scramjet, which would scoop oxygen from the atmosphere as it ascends.───有一个可能的解决方法，就是超音速燃烧冲压喷射引擎（supersoniccombustionramjet，简称scramjet），它在升空时会努力从大气吸入氧氧。

Second, the influences of cavity flame-holders in the supersonic combustion were analysed.───分析了凹腔在超声速燃烧室中的作用；

Cavity is flame holder in high turbulent supersonic combustion.───凹腔是高湍流度超声速燃烧的火焰稳定装置。

Experimental investigation of a supersonic combustion flowfield employing staged transverse injection behind a rearward-facing step───运用背风突阶后的分级横向喷射对超音速燃烧流场进行实验性研究

Numerical Simulation on Supersonic Combustion over a Reward Facing Step with Transverse Hydrogen and Air Injection───后台阶喷氢加喷空气超音速燃烧数值模拟

Experimental Study of Supersonic Combustion of Kerosene───煤油超音速燃烧的试验研究

英语使用场景

The mixture - fraction equilibrium chemistry model and discrete droplet model can predict correctly kerosene spray supersonic combustion.

The supersonic combustion chamber inlet is a 2 D convergent - divergent nozzle.

Then the influence on flame structure of supersonic combustion of ratio of length and deep of cavity, obliquity of back edge of cavity and different schemes of fuel injection were studied.

The effects of temperature and equivalence ratio of supersonic premixed combustible flow on the structure of supersonic combustion flow field, ignition and flame propagation were studied.

A new supersonic combustion ramjet, or scramjet, engine gets put through its paces at a NASA research center in a ground-based test that simulated Mach 5 conditions in 2008.