supersonic combustion的意思

supersonic combustion中文翻譯：

超音速燃燒

相似詞語短語

combustion───n.燃燒，氧化；騷動

combustion air───[熱]助燃空氣；[熱]燃燒空氣

combustion chamber───燃燒室; 爐膛；[動力]燃燒室

spontaneous combustion───n.自燃

combustion tube───[分化]燃燒管；縱火筒

internal combustion───內燃（燒）

internal combustion engine───[動力]內燃機

combustion and flame───燃燒與火焰

flamelet combustion model───小火焰燃燒模型

雙語使用場景

The mixture-fraction equilibrium chemistry model and discrete droplet model can predict correctly kerosene spray supersonic combustion.───混合分數平衡化學反應模型和離散液滴模型能準確地預測煤油在雙模態燃燒室內的噴霧燃燒。

The results show that some of technological problems for experimental investigation on supersonic combustion with shock tunnels have been solved basically.───結果表明激波風洞用于超聲速燃燒研究的一些必要的技術問題已基本解決。

Numerical analysis of the kerosene spray supersonic combustion was carried out in the dual-mode supersonic combustor with the CFD software.───計算流體力學軟件對煤油在所設計的雙模態超聲速燃燒室內的超聲速噴霧燃燒進行了數值模擬。

One answer could come from a supersonic combustion ramjet, known as a scramjet, which would scoop oxygen from the atmosphere as it ascends.───有一個可能的解決方法，就是超音速燃燒沖壓噴射引擎（supersoniccombustionramjet，簡稱scramjet），它在升空時會努力從大氣吸入氧氧。

Second, the influences of cavity flame-holders in the supersonic combustion were analysed.───分析了凹腔在超聲速燃燒室中的作用；

Cavity is flame holder in high turbulent supersonic combustion.───凹腔是高湍流度超聲速燃燒的火焰穩定裝置。

Experimental investigation of a supersonic combustion flowfield employing staged transverse injection behind a rearward-facing step───運用背風突階后的分級橫向噴射對超音速燃燒流場進行實驗性研究

Numerical Simulation on Supersonic Combustion over a Reward Facing Step with Transverse Hydrogen and Air Injection───后臺階噴氫加噴空氣超音速燃燒數值模擬

Experimental Study of Supersonic Combustion of Kerosene───煤油超音速燃燒的試驗研究

英語使用場景

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.