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Effect of characteristic structure of nested composite hybrid rocket fuel grain on combustion properties 期刊论文
ACTA ASTRONAUTICA, 2024, 卷号: 218, 页码: 269-281
Authors:  Wang RY(王若岩);  Lin X(林鑫);  Wang ZZ(王泽众);  Wu K(吴坤);  Pan JJ(潘俊杰);  Zhang ZL(张泽林);  Luo JX(罗家枭);  Li F(李飞);  Yu XL(余西龙)
Favorite  |  View/Download：18/0  |  Submit date：2024/05/21
Hybrid rocket  Composite fuel grain  Characteristic structure  Radiation image  Combustion properties  
Error Analysis of Integrated Absorbance for TDLAS in a Nonuniform Flow Field 期刊论文
APPLIED SCIENCES-BASEL, 2021, 卷号: 11, 期号: 22, 页码: 15
Authors:  Li RJ(李仁杰);  Li F(李飞);  Lin X(林鑫);  Yu XL(余西龙)
Adobe PDF(7410Kb)  |  Favorite  |  View/Download：261/47  |  Submit date：2022/01/13
TDLAS  integrated absorbance  error analysis  
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：326/61  |  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：556/72  |  Submit date：2021/08/03
Tunable diode laser absorption spectroscopy  Hybrid rocket motor  Temperature  Partial pressure  Combustion efficiency  
Reconstructing shock front of unstable detonations based on multi-layer perceptron 期刊论文
ACTA MECHANICA SINICA, 2021, 页码: 14
Authors:  Zhou, Lin;  Teng, Honghui;  Ng, Hoi Dick;  Yang PF(杨鹏飞);  Jiang ZL(姜宗林)
Adobe PDF(6382Kb)  |  Favorite  |  View/Download：241/37  |  Submit date：2021/11/01
Cellular detonation  Lead shock evolution  Multi-layer perceptron  Numerical simulations  
Fluid-structure interaction-based aerodynamic modeling for flight dynamics simulation of parafoil system 期刊论文
NONLINEAR DYNAMICS, 2021, 页码: 22
Authors:  Zhu, Hong;  Sun, Qinglin;  Liu, Xuefeng;  Liu, Jinglei;  Sun, Hao;  Wu WN(邬婉楠);  Tan, Panlong;  Chen, Zengqiang
Adobe PDF(4213Kb)  |  Favorite  |  View/Download：327/60  |  Submit date：2021/08/03
Fluid-structure interaction  Parafoil system  Flexible deformation  Trailing edge deflection  Aerodynamic performance  Dynamic model  
Improving the Combustion Performance of a Hybrid Rocket Engine using a Novel Fuel Grain with a Nested Helical Structure 期刊论文
JOVE-JOURNAL OF VISUALIZED EXPERIMENTS, 2021, 期号: 167, 页码: 17
Authors:  Wang ZZ(王泽众);  Lin X(林鑫);  Li F(李飞);  Zhang ZL(张泽林);  Yu XL(余西龙)
Adobe PDF(1456Kb)  |  Favorite  |  View/Download：290/69  |  Submit date：2021/06/15
Ideas and perspectives: the same carbon behaves like different elements - an insight into position-specific isotope distributions 期刊论文
BIOGEOSCIENCES, 2020, 卷号: 17, 期号: 19, 页码: 4785-4795
Authors:  He YY(何雨旸);  Cao XB;  Bao HM
Adobe PDF(679Kb)  |  Favorite  |  View/Download：351/59  |  Submit date：2020/11/30
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：291/110  |  Submit date：2020/05/18
Hybrid rocket engine  Paraffin-based fuel  Acrylonitrile-butadiene-styrene  Regression rate  Combustion efficiency