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
收藏
页码：190 / 198
页数：9
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