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Effects of swirl injection on the combustion of a novel composite hybrid rocket fuel grain 期刊论文
ACTA ASTRONAUTICA, 2022, 卷号: 199, 页码: 174-182
Authors:  Zhang ZL(张泽林);  Lin X(林鑫);  Wang ZZ(王泽众);  Wu K(吴坤);  Luo JX(罗家枭);  Fang SH(方思晗);  Zhang CY(张春元);  Li F(李飞);  Yu XL(余西龙)
Adobe PDF(9227Kb)  |  Favorite  |  View/Download：101/11  |  Submit date：2022/11/08
Hybrid rocket engine  Swirl injection  Novel composite fuel grain  Regression rate  Oxidizer-to-fuel ratio  
Determining the time-resolved mass flow rates of hybrid rocket fuels using laser absorption spectroscopy 期刊论文
ACTA ASTRONAUTICA, 2021, 卷号: 188, 页码: 110-120
Authors:  Wang ZZ(王泽众);  Lin X(林鑫);  Li F(李飞);  Peng JL(彭锦龙);  Liu, Yan;  Zhang ZL(张泽林);  Fang SH(方思晗);  Yu XL(余西龙)
Adobe PDF(6496Kb)  |  Favorite  |  View/Download：306/58  |  Submit date：2021/11/01
Hybrid rocket engine  Fuel mass flow rate  Tunable diode laser absorption spectroscopy  Temperature  Partial pressure  
Characterizing combustion of a hybrid rocket using laser absorption spectroscopy 期刊论文
EXPERIMENTAL THERMAL AND FLUID SCIENCE, 2021, 卷号: 127, 页码: 9
Authors:  Fang SH(方思晗);  Wang ZZ(王泽众);  Lin X(林鑫);  Li F(李飞);  Li RJ(李仁杰);  Li, Jing;  Zhang, Zhedian;  Liu, Yan;  Yu XL(余西龙)
Adobe PDF(4367Kb)  |  Favorite  |  View/Download：542/67  |  Submit date：2021/08/03
Tunable diode laser absorption spectroscopy  Hybrid rocket motor  Temperature  Partial pressure  Combustion efficiency