EXPERIMENTAL AND THEORETICAL DETERMINATION OF ADMITTANCES OF A FAMILY OF NOZZLES SUBJECTED TO AXIAL INSTABILITIES

被引：19

作者：

BELL, WA ^{[1
]}

DANIEL, BR ^{[1
]}

ZINN, BT ^{[1
]}

机构：

[1] GEORGIA INST TECHNOL,SCH AEROSP ENGN,ATLANTA,GA 30332

来源：

关键词：

D O I：

10.1016/S0022-460X(73)80112-9

中图分类号：

O42 [声学];

学科分类号：

070206 ; 082403 ;

摘要：

引用

页码：179 / 190

页数：12

共 17 条

[1]

Bell W. A., 1972, THESIS GEORGIA I TEC

[2]

BUFFUM FG, 1966, NOTSTP3932 NAV ORDN

CROCCO, L ;

MONTI, R ;

GREY, J .

ARS JOURNAL, 1961, 31 (06) :771-775

[4]

Crocco L, 1953, AEROTECHNICA, V33, P46

[5]

CROCCO L, 1965, 10 S INT COMB, P1101, DOI DOI 10.1016/S0082-0784(65)80249-1

[6]

CROCCO L, 1956, AGARD8, pCH1

[7]

CROCCO L, 1967, AGARD117

[8]

CULICK FEC, 1968, NWC4544 NAV WEAP CTR

[9]

GATELY WS, 1969, J ACOUSTICAL SOCIETY, V46, P6

[10]

LIPPERT WKR, 1953, ACUSTICA, V3, P153