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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 |