FORMATION OF SHOCKS WITHIN AXISYMMETRICAL NOZZLES

被引：6

作者：

LOTH, E ^{[1
]}

BAUM, J ^{[1
]}

LOHNER, R ^{[1
]}

机构：

[1] USN,RES LAB,COMPUTAT PHYS & FLUID DYNAM LAB,WASHINGTON,DC 20375

来源：

AIAA JOURNAL | 1992年 / 30卷 / 01期

关键词：

D O I：

10.2514/3.10909

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

[No abstract available]

引用

页码：268 / 270

页数：3

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[5] AN ADAPTIVE FINITE-ELEMENT PROCEDURE FOR COMPRESSIBLE HIGH-SPEED FLOWS [J].

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[6]

LOHNER R, 1989, AIAA891794 APA

[7]

LOTH E, 1990, AIAA901655 PAP

[8]

Oran E.S., 2001, NUMERICAL SIMULATION, V2nd ed.

[9]

ROE PL, 1987, 876 I COMP APPL SCI

[10]

SERRA J, 1972, AIAA J, V10, P603

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