ANALYSIS OF UNSTEADY TRANSONIC CHANNEL FLOW WITH SHOCK-WAVES

被引：13

作者：

RICHEY, GK

ADAMSON, TC

机构：

[1] USAF,FLIGHT DYNAM LAB,WRIGHT PATTERSON AFB,OH 45433

[2] UNIV MICHIGAN,ANN ARBOR,MI 48104

来源：

关键词：

D O I：

10.2514/3.61441

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：1054 / 1061

页数：8

共 9 条

ADAMSON, TC ;

RICHEY, GK .

[2] UNSTEADY TRANSONIC FLOWS IN 2-DIMENSIONAL CHANNELS [J].

ADAMSON, TC .

[3]

ADAMSON TC, 1974, ARCH MECH, V26, P617

[4]

GUDERLEY KG, 1962, THEORY TRANSONIC FLO, P7

[5] FLOW NEAR A WEAK SHOCK-WAVE DOWNSTREAM OF A NOZZLE THROAT [J].

MESSITER, AF ;

ADAMSON, TC .

[6]

RICHEY GK, 1975, THESIS U MICHIGAN

[7] EFFECT OF LONGITUDINAL VISCOSITY ON FLOW AT A NOZZLE THROAT [J].

SICHEL, M .

[8]

SZANIAWSKI A, 1965, ARCH MECH STOSOW, V17, P79

TOMOTIKA, S ;

TAMADA, K .