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流場周向非均勻性的動量輸運和能量輸運作用。
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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種分析進口總壓畸變對多級軸流壓氣機特性影響的逐級模擬方法。
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.
介紹了葉輪機虛擬樣機技術(shù)、多級軸流壓氣機數(shù)值仿真和葉輪機與發(fā)動機一體化設(shè)計。