文章基本信息

标题：Computational simulation of multi-strut central lobed injection of hydrogen in a scramjet combustor
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作者：Gautam Choubey ; Gautam Choubey ; K.M. Pandey 等
期刊名称：Perspectives in Science
印刷版ISSN：2213-0209
电子版ISSN：2213-0209
出版年度：2016
卷号：8
页码：222-224
DOI：10.1016/j.pisc.2016.04.032
语种：English
出版社：Elsevier
摘要：Summary Multi-strut injection is an approach to increase the overall performance of Scramjet while reducing the risk of thermal choking in a supersonic combustor. Hence computational simulation of Scramjet combustor at Mach 2.5 through multiple central lobed struts (three struts) have been presented and discussed in the present research article. The geometry and model used here is slight modification of the DLR (German Aerospace Center) scramjet model. Present results show that the presence of three struts injector improves the performance of scramjet combustor as compared to single strut injector. The combustion efficiency is also found to be highest in case of three strut fuel injection system. In order to validate the results, the numerical data for single strut injection is compared with experimental result which is taken from the literature.
关键词：CFD; Scramjet; Combustion efficiency; Supersonic combustion;