Numerical simulation of impinging jet produced by missile

被引：0
|
作者：
Jiguo, Sun [1 ]
Jue, Wang [1 ]
机构：
[1] Beijing Fengyuan Machinery Inst., Beijing 100076, China
来源：
Tuijin Jishu/Journal of Propulsion Technology | 2000年 / 21卷 / 01期
关键词：
Computer simulation - Difference equations - Exhaust systems (engine) - Jets - Missiles - Navier Stokes equations - Thermal plumes;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Impinging jet produced by launching missile was numerically simulated by using NND2M difference scheme which was simple structure and efficient to use. The computation was based on the Navier-Stokes equations. The computational results were well agreement with the experimental results. Then the flow structure was studied.
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页码：30 / 32
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