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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：330/62  |  Submit date：2021/11/01
Hybrid rocket engine  Fuel mass flow rate  Tunable diode laser absorption spectroscopy  Temperature  Partial pressure  
Synthesis and characterization of light-weight porous ceramics used in the transpiration cooling 期刊论文
ACTA ASTRONAUTICA, 2020, 卷号: 177, 页码: 438-445
Authors:  Zhang, Bo;  Huang, Jie;  Li, Weijie;  Huang, Haiming;  Zhao, Huanyu;  Peng JL(彭锦龙)
Adobe PDF(8097Kb)  |  Favorite  |  View/Download：407/83  |  Submit date：2021/03/30
Carbon fiber-reinforced silicon carbide porous ceramics  Permeability  Oxyacetylene flame test  Transpiration cooling  
Numerical study on supersonic boundary-layer transition and wall skin friction reduction induced by fuel wall-jet combustion 期刊论文
ACTA ASTRONAUTICA, 2020, 卷号: 174, 页码: 11-23
Authors:  Xue R;  Zheng X;  Yue LJ(岳连捷);  Zhang SK;  Weng C
Adobe PDF(3912Kb)  |  Favorite  |  View/Download：356/239  |  Submit date：2020/08/26
Compressible boundary layer combustion  Skin-friction reduction  Boundary layer transition  Transition k-kl-w model  Hydrogen combustion  
Parametric study on drag reduction with the combination of the upstream energy deposition and the opposing jet configuration in supersonic flows 期刊论文
ACTA ASTRONAUTICA, 2020, 卷号: 171, 页码: 300-310
Authors:  Ju SJ;  Sun ZX(孙振旭);  Yang GW(杨国伟);  Prapamonthon P;  Zhang JY
Adobe PDF(3216Kb)  |  Favorite  |  View/Download：356/94  |  Submit date：2020/05/18
Computational fluid dynamics  Drag reduction  Supersonic flow  Energy deposition  Opposing jet  
Numerical study on the aerothermodynamics of different heatshield configurations for Mars entry capsules 期刊论文
ACTA ASTRONAUTICA, 2019, 卷号: 157, 页码: 189-198
Authors:  Zhong K;  Yan C;  Chen SS;  Wang XY(王小永);  Ju SJ
View  |  Adobe PDF(8635Kb)  |  Favorite  |  View/Download：250/74  |  Submit date：2019/05/29
Aeroheating  Heatshield configuration  Sphere-cone angle  Mars  Turbulent