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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
作者:  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)  |  收藏  |  浏览/下载:279/51  |  提交时间:2021/11/01
Hybrid rocket engine  Fuel mass flow rate  Tunable diode laser absorption spectroscopy  Temperature  Partial pressure  
Shock wave and turbulent boundary layer interaction in a double compression ramp 期刊论文
COMPUTERS & FLUIDS, 2021, 卷号: 229, 页码: 15
作者:  Tong FL(童福林);  Duan JY(段俊亦);  Li XL(李新亮)
Adobe PDF(10792Kb)  |  收藏  |  浏览/下载:267/39  |  提交时间:2021/11/01
Shock wave  Turbulent boundary layer  Double compression ramp  Direct numerical simulation  
Direct numerical simulation of a supersonic turbulent boundary layer over a compression–decompression corner 期刊论文
Physics of Fluids, 2021, 卷号: 33, 页码: 065111
作者:  段俊亦;  李欣;  李新亮;  刘洪伟
Adobe PDF(5069Kb)  |  收藏  |  浏览/下载:173/44  |  提交时间:2021/11/23
Advances in critical technologies for hypersonic and high-enthalpy wind tunnel 期刊论文
CHINESE JOURNAL OF AERONAUTICS, 2020, 卷号: 33, 期号: 12, 页码: 3027-3038
作者:  Jiang ZL(姜宗林);  Hu ZM(胡宗民);  Wang YP(汪运鹏);  Han GL(韩桂来)
Adobe PDF(1129Kb)  |  收藏  |  浏览/下载:326/169  |  提交时间:2021/03/30
High-enthalpy flow  Hypersonic wind tunnel  Aerospace vehicle  Aerodynamic balance  Heat flux sensor  Optical measurement technique  
Incident shock wave and supersonic turbulent boundarylayer interactions near an expansion corner 期刊论文
COMPUTERS & FLUIDS, 2020, 卷号: 198, 页码: 18
作者:  Tong FL(童福林);  Li XL(李新亮);  Yuan XX;  Yu ZP(于长平)
浏览  |  Adobe PDF(7909Kb)  |  收藏  |  浏览/下载:355/113  |  提交时间:2020/04/07
Shock wave  Turbulent boundary layer  Unsteadiness  Expansion corner  
超声速膨胀角入射激波/湍流边界层干扰直接数值模拟研究 期刊论文
航空学报, 2019, 页码: 21
作者:  童福林;  孙东;  袁先旭;  李新亮
浏览  |  Adobe PDF(1603Kb)  |  收藏  |  浏览/下载:193/66  |  提交时间:2019/12/16
激波/湍流边界层干扰  膨胀角  本征正交分解  直接数值模拟  
External-Compression Supersonic Inlet Free from Violent Buzz 期刊论文
AIAA JOURNAL, 2019, 卷号: 57, 期号: 6, 页码: 2513-2523
作者:  Chen H;  Tan H;  Liu YZ;  Zhang QF(张启帆)
浏览  |  Adobe PDF(4679Kb)  |  收藏  |  浏览/下载:271/97  |  提交时间:2019/09/09
Combustion states distinction of the methane/oxygen laminar co-flow diffusion flame at high pressure 期刊论文
FUEL, 2019, 卷号: 243, 页码: 221-229
作者:  Ge YF(葛逸飞);  Li S(李森);  Wei XL(魏小林)
浏览  |  Adobe PDF(5239Kb)  |  收藏  |  浏览/下载:355/128  |  提交时间:2019/04/11
Diffusion flame  Co-flow  Laminar  Pulsation  High pressure  
Influences of Domain Symmetry on Supersonic Combustion Modeling 期刊论文
JOURNAL OF PROPULSION AND POWER, 2019, 卷号: 35, 期号: 2, 页码: 451-465
作者:  Yao W(姚卫);  Wu K(吴坤);  Fan XJ(范学军)
Adobe PDF(862Kb)  |  收藏  |  浏览/下载:324/98  |  提交时间:2019/04/11
Numerical study on supersonic combustion of hydrogen and its mixture with Ethylene and methane with strut injection 期刊论文
INTERNATIONAL JOURNAL OF HYDROGEN ENERGY, 2018, 卷号: 43, 期号: 15, 页码: 7591-7599
作者:  Ma SG(马素刚);  Zhong FQ(仲峰泉);  Zhang XY(张新宇)
浏览  |  Adobe PDF(2634Kb)  |  收藏  |  浏览/下载:268/112  |  提交时间:2018/07/17
Detached Eddy Simulation  Reduced Kinetic Mechanism  Supersonic Combustion  Hydrogen  Hydrocarbon