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Simulation of kerosene fueled RBCC engine based on skeletal mechanism

  • Northwestern Polytechnical University Xian

科研成果: 书/报告/会议事项章节会议稿件同行评审

6 引用 (Scopus)

摘要

The detailed kerosene high temperature mechanism of C10H22 consisting of 121 species 866 elemental reactions is reduced by DRG method and CSP importance index. A skeletal chemical mechanism of kerosene containing 41 species and 132 elemental reactions is finally obtained. The comparisons of flame temperature, ignition delay time, ignition process and extinction predicted by the skeletal mechanism show an overall good accordance with the detailed reaction mechanism. Moreover, a three-dimensional RANS modeling based on the skeletal kerosene mechanism and a global reaction with the single compound C11H21 is employed for the numerical analysis of a full-scale RBCC engine, which has been experimentally tested in a direct connect supersonic combustion test platform assembled in Science and Technology on Combustion, Internal Flow and Thermal-structure Laboratory (Northwestern Polytechnical University, Xi’an, China). Both the skeletal mechanism and C11H21 global reaction can demonstrate appropriate accuracy with the experiment result.

源语言英语
主期刊名21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017
出版商American Institute of Aeronautics and Astronautics Inc, AIAA
ISBN(印刷版)9781624104633
DOI
出版状态已出版 - 2017
活动21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017 - Xiamen, 中国
期限: 6 3月 20179 3月 2017

出版系列

姓名21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017

会议

会议21st AIAA International Space Planes and Hypersonics Technologies Conference, Hypersonics 2017
国家/地区中国
Xiamen
时期6/03/179/03/17

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