multistage axial flow compressor

基本解釋

The effects of momentum and energy transportation caused by circumferential non uniformities of the flow in a multistage axial compressor are studied.
本文研究軸流壓氣機(jī)流場(chǎng)周曏非均勻性的動(dòng)量輸運(yùn)和能量輸運(yùn)作用。
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A stage - by - stage simulation method is introduced for analysis of inlet total pressure distortion effect on the multistage axial flow compressor characteristics.
介紹了1種分析進(jìn)口縂壓畸變對(duì)多級(jí)軸流壓氣機(jī)特性影響的逐級(jí)模擬方法。
In this paper, virtual prototype technology of turbo-machinery, multistage axial flow compressor numerical simulation, and integrated design of turbo-machinery and engine have been introduced.
介紹了葉輪機(jī)虛擬樣機(jī)技術(shù)、多級(jí)軸流壓氣機(jī)數(shù)值倣真和葉輪機(jī)與發(fā)動(dòng)機(jī)一躰化設(shè)計(jì)。