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Reactive Fields Analysis of Hybrid Combustor Under Different Arrangements of Oxidizer Injectors  

Cho Sung-Chan (한국항공대학교 항공우주 및 기계공학과)
Kim Soo-Jong (한국항공대학교 항공우주 및 기계공학과)
Lee Seung-Chul (한국항공대학교 항공우주 및 기계공학과)
Kim Jin-Kon (한국항공대학교 항공우주 및 기계공학과)
Koo Ja-Yae (한국항공대학교 항공우주 및 기계공학과)
Moon Hee-Jang (한국항공대학교 항공우주 및 기계공학과)
Publication Information
Journal of the Korean Society of Propulsion Engineers / v.9, no.2, 2005 , pp. 78-88 More about this Journal
Abstract
The combustion characteristics of End-Burning hybrid combustor using different types of injector system are numerically investigated to visualize the temperature fields in the combustion chamber The basic characteristics of combustion with different O/F ratio is also analyzed in order to capture the main behavior of diffusion flame inside the swirl induced hybrid combustion chamber It was found that the arrangement of oxidizer injectors give strong effect on the temperature field dominating mixing between fuel and oxidizer. The results show that among five different oxidizer injectors arrangement, the counter flow injector has the highest mixing efficiency. However, the observed high wall temperature presence near the oxidizer injectors remains to be solved.
Keywords
End-Burning Combustor; Hybrid Combustion; O/F Ratio; Oxidizer Injector;
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