AN ANALYTICAL DESCRIPTION OF UNSTEADY TRANSONIC LAVAL-NOZZLE FLOW

被引：0

作者：

OBERMEIER, F

机构：

[1] Max-Planck-Inst fuer, Stroemungsforschung, Germany

来源：

ZEITSCHRIFT FUR FLUGWISSENSCHAFTEN UND WELTRAUMFORSCHUNG | 1988年 / 12卷 / 04期

关键词：

D O I：

暂无

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

引用

页码：253 / 257

页数：5

共 14 条

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[7]

MEIER GEA, 1976, S TRANSSONICUM, V2, P252

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

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ADAMSON, TC .

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[9] KINEMATICS OF A MULTIDIMENSIONAL SHOCK OF ARBITRARY STRENGTH IN AN IDEAL-GAS [J].

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[10]

Pritulo M. F., 1962, PMM-J APPL MATH MEC, V26, P661

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