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NO激光诱导荧光对高焓气流温度的测量 期刊论文
气体物理, 2020, 卷号: 5, 期号: 02, 页码: 1-7
Authors:  严浩;  张少华;  王方仪;  余西龙
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高焓气流  激光诱导荧光  NO  激波风洞  双线测温法  
Combustion performance of a novel hybrid rocket fuel grain with a nested helical structure 期刊论文
AEROSPACE SCIENCE AND TECHNOLOGY, 2020, 卷号: 97, 页码: 8
Authors:  Wang ZZ(王泽众);  Lin X(林鑫);  Li F(李飞);  Yu XL(余西龙)
Adobe PDF(1961Kb)  |  Favorite  |  View/Download：285/108  |  Submit date：2020/05/18
Hybrid rocket engine  Paraffin-based fuel  Acrylonitrile-butadiene-styrene  Regression rate  Combustion efficiency  
A method for rapid generation of 3D infrared radiation intensity field of engine exhaust plume 会议论文
6th Symposium on Novel Optoelectronic Detection Technology and Applications, Beijing, PEOPLES R CHINA, 3 December 2019 through 5 December 2019
Authors:  Bao XD(包醒东);  Yu XL(余西龙);  Wang Z.-H;  Mao H.-X;  Xiao Z.-H.
Adobe PDF(602Kb)  |  Favorite  |  View/Download：173/76  |  Submit date：2021/06/11
Calculation method  Exhaust plume  Infrared spectroscopy  Radiation intensity  Three-dimensional space  
Temperature and H2O concentration measurements for a hybrid rocket motor plume using a single mid-infrared tunable diode laser 会议论文
2020 Applied Optics and Photonics China: Optical Sensing and Imaging Technology, AOPC 2020, Xiamen, PEOPLES R CHINA, 25 August 2020 through 27 August 2020
Authors:  Fang SH(方思晗);  Wang ZZ(王泽众);  Li RJ(李仁杰);  Zhang ZL(张泽林);  Lin X(林鑫);  Li F(李飞);  Yu XL(余西龙)
Adobe PDF(1569Kb)  |  Favorite  |  View/Download：224/67  |  Submit date：2021/06/11
concentration  hybrid rocket motor  nozzle exit  temperature  Tunable diode laser absorption spectroscopy (TDLAS)  water vapor