Analysis of thermal choking in expanding RBCC duct

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

Expanding combustor has been validated to realize the best performance of the RBCC engine which has several operating modes. But it is based on the implementation of thermal choking in the duct which was influenced by several factors including expanding angle, heating amount and heating rate etc. A theoretical one dimensional model was developed in this paper to describe the flow in an expanding duct. it is concluded by the one-dimensional analysis that the expanding angle, heating increment and heat release law are of crucial effect on the thermal choking. These factors mainly influence the position of choking throat, the total pressure loss and distribution of the temperature. In order to implement thermal choking in the duct, there must be a certain heat release law, heating increment and a special expanding angle which depends on the given heating law. In order to transit subsonic flow to supersonic flow in expanding duct, the heating rate should change from a bigger value to a smaller one.

源语言英语
主期刊名60th International Astronautical Congress 2009, IAC 2009
6461-6470
页数10
出版状态已出版 - 2009
活动60th International Astronautical Congress 2009, IAC 2009 - Daejeon, 韩国
期限: 12 10月 200916 10月 2009

出版系列

姓名60th International Astronautical Congress 2009, IAC 2009
8

会议

会议60th International Astronautical Congress 2009, IAC 2009
国家/地区韩国
Daejeon
时期12/10/0916/10/09

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