文章基本信息

标题：Flow Parameters Behind an Unsteady Curved Shock Wave in an Ideal Gas with Heat Addition
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作者：B. G. Verma
期刊名称：Defence Science Journal
印刷版ISSN：0976-464X
出版年度：2014
卷号：17
期号：3
页码：145-150
DOI：10.14429/dsj.17.7384
语种：English
出版社：Defence Scientific Information & Documentation Centre
摘要：This paper discusses the flows immediately behind and in front of a two dimensional unsteady curved shock wave in an ideal gas with heat addition. Method evolved by Thomas has been followed to obtain formulas for the determination of the gradients of velocity components, pressure and density behind the shock when the flow in front is known.
关键词：Curved Shock Wave