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Propagation of pressure wave in a pulsed T-burner

  • Beijing Institute of Technology

科研成果: 书/报告/会议事项章节 › 会议稿件 › 同行评审

摘要

Based on the Su's T-burner test, the numerical simulation method has been used to study the propagation of pressure wave after a pulse, aiming to explore the pressure waveform characteristics after pulse and to provide a corresponding theoretical guidance to the future experiments. The calculated results are consistent well with the experimental values. Several cases of different waveforms stages after pulse have been presented to investigate the waveform conversion process. The results indicate that there is a waveform conversion process in the combustion instability process. The characteristics of this process has been analyzed and categorized. The conversion process has been divided into five steps in the whole process. There are great differences in both pressure and temperature waveforms in different transition stage. This differences may lead to some significant impact on the final result in the related test and the characteristics of the chamber. In order to predict the combustion instability of the SRM accurately, the waveform of the chamber pressure is necessary to consider.

源语言英语
主期刊名53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017
出版商American Institute of Aeronautics and Astronautics Inc, AIAA
ISBN(印刷版)9781624105111
DOI
出版状态已出版 - 2017
活动53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017 - Atlanta, 格鲁吉亚
期限: 10 7月 2017 → 12 7月 2017

丛书

姓名53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017

会议

会议53rd AIAA/SAE/ASEE Joint Propulsion Conference, 2017
国家/地区格鲁吉亚
市Atlanta
时期10/07/17 → 12/07/17

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