VISCOUS INVISCID ANALYSIS OF CURVED SUBSONIC OR SUPERSONIC WALL JETS

被引：9

作者：

DASH, SM

BEDDINI, RA

WOLF, DE

SINHA, N

机构：

[1] Science Applications Inc, Princeton,, NJ, USA, Science Applications Inc, Princeton, NJ, USA

来源：

AIAA JOURNAL | 1985年 / 23卷 / 01期

关键词：

CIRCULATION-CONTROLLED AIRFOIL - MULTIPLE-CELL SHOCK STRUCTURE - PRESSURE SPLIT CURVED WALL JET MODEL - VISCOUS-INVISCID ANALYSIS;

D O I：

10.2514/3.8865

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：12 / 13

页数：2

共 11 条

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[5]

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[10] CALCULATION OF TURBULENT-INVISCID FLOW INTERACTIONS WITH LARGE NORMAL PRESSURE-GRADIENTS [J].

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BRADSHAW, P .

AIAA JOURNAL, 1979, 17 (10) :1025-1029

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