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

被引：491

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

共 14 条

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[2]

GREITZER EM, SURGE ROTATING STA 2

[3]

GREITZER EM, 1972, FURTHER INVESTIGATIO

[4]

HALFMAN RL, 1962, DYNAMICS, V1, pCH7

[5]

HORLOCK JH, 1958, AXIAL FLOW COMPRESSO, pCH7

[6] SOME STALL AND SURGE PHENOMENA IN AXIAL-FLOW COMPRESSORS [J].

HUPPERT, MC ;

BENSER, WA .

JOURNAL OF THE AERONAUTICAL SCIENCES, 1953, 20 (12) :835-845

[7]

HUPPERT MC, 1965, SP36 NASA, pCH12

[8]

MARSH H, 1973, 3 I MECH ENGRS C PUB

[9]

MCLACHLAN NW, 1956, ORDINARY NONLINEAR D, pCH6

[10]

PEARSON CE, 1954, 142 PRATT WHITN RES