Numerical Simulation of Laval Nozzle

被引：0

作者：

Wang Yandong ^{[1
]}

Jia Hongguang ^{[1
]}

机构：

[1] Chinese Acad Sci, CIOMP, Changchun, Jilin, Peoples R China

来源：

ADVANCED DESIGN AND MANUFACTURING TECHNOLOGY III, PTS 1-4 | 2013年 / 397-400卷

关键词：

Laval nozzle; simulation; control equation;

D O I：

10.4028/www.scientific.net/AMM.397-400.266

中图分类号：

TP39 [计算机的应用];

学科分类号：

081203 ; 0835 ;

摘要：

Laval nozzle is the commonly used device in rocket engine and aero engine, this paper, the numerical model is derived. The convergent section subsonic flow and divergent section hypersonic flow are simulated in dimensionless method. Reverting the dimension, the result can be seen that the analytical solution, the CFX simulation solution and the numerical are in uniform.

引用

页码：266 / 269

页数：4

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