Numerical Simulation of Supersonic Axisymmetric Gas Jets

被引：1
|
作者：
Yu. N. Sadkov
机构：
来源：
Computational Mathematics and Modeling | 2004年 / 15卷 / 4期
关键词：
Mathematical Modeling; Equation Model; Computational Mathematic; Industrial Mathematic; Difference Scheme;
D O I：
10.1023/B:COMI.0000047344.94959.bb
中图分类号：
学科分类号：
摘要：
The oscillations of free supersonic jets are simulated using the axisymmetric Euler equation model. A third order accurate through difference scheme with artificial viscosity is used. Jet flows from a sonic nozzle with nozzle-to-ambient pressure ratio between 1.2 and 2 are investigated. The numerical results are compared with physical experiments.
引用
收藏
页码：344 / 349
页数：5
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