Experimental study on flow distribution in micro backflow combustor

Experimental study on flow distribution in micro backflow combustor

Junli Yu Chungang Qu Xuan Wang 

Civil Aviation University of China, College of Aeronautical Engineering, Tianjin 300300, China

Corresponding Author Email: 
pqbird@sina.com
Page: 
1010-1014
|
DOI: 
https://doi.org/10.18280/ijht.360330
Received: 
18 December 2017
| |
Accepted: 
15 May 2018
| | Citation

OPEN ACCESS

Abstract: 

Based on the measurement principle of plugging method and the changes in the relationship between temperature and resistance of thermistor, this study explores the flow distribution of backflow combustor of a micro jet engine. The experimental results show that with the increase of the inlet flow of the combustion, the flow distribution of different airflow channels on the wall of the flame tube will change in the micro backflow combustor. When the combustor’s inlet flow is relatively large, the flow distribution approaches to the value calculated by the area method. At the same time, the experimental results show that this method is suitable for the study of flow distribution.

Keywords: 

flow distribution, backflow combustor, plugging method, thermistor, micro jet engine

1. Introduction
2. Test Model
3. Measurement Principle of Test
4. Test Results and Analysis
5. Conclusions
Acknowledgements

Basic scientific research fee project of central colleges and universities (3122015C009); Experimental technological innovation fund (02-14-01); Scientific research startup fund project (2011QD07S).

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