UNSTEADY-FLOW IN A SUPERSONIC CASCADE WITH SUBSONIC LEADING-EDGE LOCUS

被引：43

作者：

ADAMCZYK, JJ

GOLDSTEIN, ME

机构：

来源：

关键词：

D O I：

10.2514/3.61040

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：1248 / 1254

页数：7

共 15 条

[1]

BRIX CW, 1974, AIAA7414 PAP

[2]

FUNG YC, 1955, INTRO THEORY AEROELA, P166

GOLDSTEIN, ME ;

BRAUN, W ;

ADAMCZYK, JJ .

[4] CASCADE WITH SUBSONIC LEADING-EDGE LOCUS [J].

GOLDSTEIN, ME .

[5]

GOLDSTEIN ME, 1975, X71673 NASA TM

[6] ISSUE OF RESONANCE IN AN UNSTEADY SUPERSONIC CASCADE [J].

KUROSAKA, M .

[7]

KUROSAKA M, 1974, T AM SOC MECH ENG, V96, P13

[8] SYSTEM MODE SHAPES IN THE FLUTTER OF COMPRESSOR BLADE ROWS [J].

LANE, F .

JOURNAL OF THE AERONAUTICAL SCIENCES, 1956, 23 (01) :54-66

[9]

LANE F, 1958, TR4136 NACA

[10] SOUND TRANSMISSION THROUGH BLADE ROWS [J].

MANI, R ;

HORVAY, G .