The Stacking of Compressor Stage Characteristics to Give an Overall Compressor Performance Map

The Stacking of Compressor Stage Characteristics to Give an Overall Compressor Performance Map
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DOI:
10.1017/s0001925900002560
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发表时间:
1962-11
期刊:
The Aeronautical Quarterly
影响因子:
--
通讯作者:
M. D. C. Doyle;S. L. Dixon
M. D. C. Doyle;S. L. Dixon
中科院分区:
其他
文献类型:
--
作者:
M. D. C. Doyle;S. L. Dixon

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开发了一种计算方法,通过“叠加”技术,根据各个级特性的知识来计算多级轴流压缩机的整体性能。设计压缩机模型并计算其整体性能。对这些结果进行比较,定性地显示设计和舞台性能的改变对整体性能的影响,并找出如何设计压缩机以获得最佳性能。
A method of calculation is developed to compute the overall performance of a multi-stage axial compressor, from a knowledge of the individual stage characteristics, by a “stacking” technique. Compressor models are designed and their overall performance calculated. These results are compared to show, qualitatively, the effect of alterations in design and stage performance on overall performance and to find how compressors should be designed for optimum performance.