EFFECTS OF TRAILING VORTICITY ON FLOW THROUGH HIGHLY LOADED CASCADES

被引：9

作者：

MCCUNE, JE

HAWTHORNE, WR

机构：

[1] MIT,GAS TURBINE LAB,CAMBRIDGE,MA 02139

[2] UNIV CAMBRIDGE,DEPT ENGN,CAMBRIDGE,ENGLAND

来源：

关键词：

D O I：

10.1017/S0022112076002024

中图分类号：

O3 [力学];

学科分类号：

08 ; 0801 ;

摘要：

引用

页码：721 / 740

页数：20

共 21 条

[1]

[Anonymous], 1960, INCOMPRESSIBLE AEROD

BRAGG, SL ;

HAWTHORNE, WR .

JOURNAL OF THE AERONAUTICAL SCIENCES, 1950, 17 (04) :243-249

[3]

CHENG WK, 1975, THESIS MIT

[4]

FALCAO A, 1970, THESIS CAMBRIDGE U

[5]

Hawthorne W.R., 1967, FLUID MECHANICS INTE, P238

[6]

LIGHTHILL MJ, 1958, INTRO FOURIER ANALYS

MCCUNE, JE .

JOURNAL OF THE AEROSPACE SCIENCES, 1958, 25 (09) :544-560

[8] THE TRANSONIC FLOW FIELD OF AN AXIAL COMPRESSOR BLADE ROW [J].

MCCUNE, JE .

JOURNAL OF THE AEROSPACE SCIENCES, 1958, 25 (10) :616-626

[9]

MCCUNE JE, 1970, SP304 NASA SPEC PU 1, P155

[10]

MCCUNE JE, 1972, MIT110 GAS TURB LAB