A Numerical Approach to Single and Twin Supersonic Jet Flows

E Rathakrishnan

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A Numerical Approach to Single and Twin Supersonic Jet Flows

机译：单和双超音速射流的数值方法

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摘要

This paper presents the main features of under and over expanded single and twin supersonic jet flow fields obtained with MacCormack's scheme. The present results are in good agreement with results obtained from other techniques.

机译：本文介绍了通过MacCormack方案获得的单，双超音速射流流场的上下扩展特征。目前的结果与从其他技术获得的结果非常吻合。

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来源
《Journal of the Institution of Engineers (Inida). Aerospace Engineering Division Board》 |2003年第11期|p.32-34|共3页
作者
E Rathakrishnan;
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作者单位

Department of Aerospace Engineering, Indian Institute of Technology, Kanpur 208 016;

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原文格式 PDF
正文语种 eng
中图分类无线电电子学、电信技术;
关键词
free jet; mach disc; jet boundary; supersonic;

机译：自由射流;马赫盘;射流边界;超音速;

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A Numerical Approach to Single and Twin Supersonic Jet Flows

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