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INVESTIGATION OF THE EFFECT OF VELOCITY DIAGRAM PARAMETERS ON INLET TOTAL-PRESSURE DISTORTIONS THROUGH SINGLE STAGE SUBSONIC AXIAL FLOW COMPRESSORS

机译：通过单级次轴流式压缩机研究速度图参数对进口总压力失真影响的研究

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作者
ASHBY, G. C., JR.;
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年度 1957
页码 1-53
总页数 53
原文格式 PDF
正文语种 eng
中图分类工业技术;
关键词
AXIAL FLOW; COMPRESSORS; INLET PRESSURE; SUBSONIC FLOW; VELOCITY DISTRIBUTION; GAS TURBINES; GRAPHS (CHARTS); PRESSURE GRADIENTS;

机译：轴流;压缩机;进口压力; sUBsONIC FLOW;速度分布;燃气轮机;图表（图表）;压力梯度;

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4. Experimental investigation and analysis of an axial compressor stage with 45° circumferential inlet flow pressure distortion [C] . J. Huang, H.Wu, W.H. Du International Conference on Fluid Mechanics; 20070815-19; Shanghai(CN) . 2007

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8. Investigation of the effect of velocity diagram on inlet total-pressure distortions through single-stage subsonic axial-flow compressors [R] . Ashby, George C , Jr 1957

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INVESTIGATION OF THE EFFECT OF VELOCITY DIAGRAM PARAMETERS ON INLET TOTAL-PRESSURE DISTORTIONS THROUGH SINGLE STAGE SUBSONIC AXIAL FLOW COMPRESSORS

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