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Numerical analysis of the flow field in the nozzle of hot water rocket motor

科研成果: 书/报告/会议事项章节会议稿件同行评审

摘要

Flashing is an important factor in the working process of hot water rocket motor. In order to deeply understand the performance characteristic of hot water rocket motor, a numerical simulation model of the flow field in the nozzle was established in this paper. According to the study of flow field in the nozzle of the motor,it is found that the phase change occurs at the position of the throat,and the flow reaches to supersonic after the throat because of the changing sound speed.The flow in the nozzle can be divided into three processes in this paper: single-phase flow process, flash process and expand-accelerating process.

源语言英语
主期刊名Mechanical and Aerospace Engineering V
出版商Trans Tech Publications Ltd.
635-639
页数5
ISBN(印刷版)9783038352235
DOI
出版状态已出版 - 2014
活动5th International Conference on Mechanical and Aerospace Engineering, ICMAE 2014 - Madrid, 西班牙
期限: 18 7月 201419 7月 2014

出版系列

姓名Advanced Materials Research
1016
ISSN(印刷版)1022-6680
ISSN(电子版)1662-8985

会议

会议5th International Conference on Mechanical and Aerospace Engineering, ICMAE 2014
国家/地区西班牙
Madrid
时期18/07/1419/07/14

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