SURGE AND ROTATING STALL IN AXIAL-FLOW COMPRESSORS .1. THEORETICAL COMPRESSION SYSTEM MODEL

被引：0

作者：

GREITZER, EM ^{[1
]}

机构：

[1] PRATT & WHITNEY AIRCRAFT, E HARTFORD, CT 06108 USA

来源：

MECHANICAL ENGINEERING | 1975年 / 97卷 / 05期

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D O I：

暂无

中图分类号：

TH [机械、仪表工业];

学科分类号：

0802 ;

摘要：

引用

页码：53 / 53

页数：1

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