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

被引：459

作者：

GREITZER, EM ^{[1
]}

机构：

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

来源：

JOURNAL OF ENGINEERING FOR POWER-TRANSACTIONS OF THE ASME | 1976年 / 98卷 / 02期

关键词：

D O I：

10.1115/1.3446138

中图分类号：

TM [电工技术]; TN [电子技术、通信技术];

学科分类号：

0808 ; 0809 ;

摘要：

引用

页码：190 / 198

页数：9

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