EXPERIMENTAL INVESTIGATION OF TURBULENT TRANSONIC VISCOUS-INVISCID INTERACTIONS

被引：23

作者：

ALBER, IE

BACON, JW

MASSON, BS

COLLINS, DJ

机构：

[1] TRW SYST,FLUID MECH LAB,REDONDO BEACH,CA 90278

[2] NORTHROP AEROPHYS LAB,HAWTHORNE,CA 90250

[3] AEROSP CORP,EL SEGUNDO,CA 90245

[4] CALTECH,JET PROP LAB,PASADENA,CA 91103

来源：

AIAA JOURNAL | 1973年 / 11卷 / 05期

关键词：

D O I：

10.2514/3.50501

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：620 / 627

页数：8

共 20 条

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ACKERET J, 1947, TM1113 NACA INVEST C

[2]

ALBER IE, 1971, AIAA71565 PAP

[3]

ALBER IE, 1969, AIAA69689 PAP

[4]

ALBER IE, 1971, AIAA71203 PAP

[5]

ALLEN HJ, 1945, TR833 NACA GEN THEOR

[6]

BEHRENS W, 1971, AIAA 71127 PAP

[7] THE LAW OF THE WAKE IN THE TURBULENT BOUNDARY LAYER [J].

COLES, D .

JOURNAL OF FLUID MECHANICS, 1956, 1 (02) :191-226

[8]

COLES D, 1969, 1968 P AFOSRIFP STAN, V2

[9] SUPERSONIC SEPARATED AND REATTACHING LAMINAR FLOWS .1. GENERAL THEORY AND APPLICATION TO ADIABATIC BOUNDARY-LAYER-SHOCK-WAVE INTERACTIONS [J].

LEES, L ;

REEVES, BL .

AIAA JOURNAL, 1964, 2 (11) :1907-1920

[10]

LEES L, 1970, TR7097 SAMSO TRW SYS

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