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| Experimental Study of Ignition and Flame Characteristics of Surrogate of Cracked Hydrocarbon Fuels in Supersonic Crossflow 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017 作者: Cheng LW(程柳维); Zhong FQ(仲峰泉); Wang ZP(王知溥); Gu HB(顾洪斌); Ma SG(马素刚); Zhang XY(张新宇) 浏览  |  Adobe PDF(517Kb)  |  收藏  |  浏览/下载:310/100  |  提交时间:2018/01/16 Combustors Cracks Diesel Engines Efficiency Ethylene Fighter Aircraft Fuels High Speed Cameras Ignition Kerosene Luminance Spacecraft Stabilization |
| LES Study of Flame Stabilization in DLR Hydrogen Supersonic Combustor with Strut Injection 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017 作者: Wu K(吴坤); Zhang P(张鹏); Yao W(姚卫); Fan XJ(范学军); Zhang, Peng(pengzhang.zhang@polyu.edu.hk) 浏览  |  Adobe PDF(1249Kb)  |  收藏  |  浏览/下载:300/89  |  提交时间:2018/01/16 Combustion Diesel Engines Hydrogen Large Eddy Simulation Spacecraft Stabilization Supersonic Aircraft Temperature Measurement Wall Flow |
| Downstream pressure variation induced hysteresis in the scramjet isolator 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017 作者: Huang TL(黄庭隆); Yue LJ(岳连捷); Ma SH; Jia YN(贾轶南); Zhang XY(张新宇); Yue, Lianjie(yuelj@imech.ac.cn) 浏览  |  Adobe PDF(704Kb)  |  收藏  |  浏览/下载:258/89  |  提交时间:2018/01/16 Spacecraft |
| Experimental Studies of Film Cooling in Supersonic Combustors 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017 作者: Fan C(樊川); Wang J(王晶); Fan XJ(范学军) 浏览  |  Adobe PDF(735Kb)  |  收藏  |  浏览/下载:308/101  |  提交时间:2018/01/16 Combustion Combustors Coolants Kerosene Spacecraft Supersonic Aerodynamics |
| The Phenomena of Sudden Change in Hypersonic Inlets Self-Starting Capability 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017 作者: Jia YN(贾轶南); Yue LJ(岳连捷); Zhang XY(张新宇); Jia, Yinan(yuelj@imech.ac.cn) 浏览  |  Adobe PDF(566Kb)  |  收藏  |  浏览/下载:326/71  |  提交时间:2018/01/16 Boundary Layer Flow Boundary Layers Spacecraft Wind Tunnels |
| Multispecies Absorption Measurement in an Ammonium Dinitramide based Thruster 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017 作者: Zeng W(曾徽); Lin X(林鑫); Zhen RP; Chen LZ; Li F(李飞); Yu XL(余西龙); Li, Fei(lifei@imech.ac.cn) 浏览  |  Adobe PDF(897Kb)  |  收藏  |  浏览/下载:451/97  |  提交时间:2018/01/16 Combustion Gas Absorption Infrared Devices Monopropellants Optical Parametric Oscillators Spacecraft |
| Pressure and Heat Flux Calibration of the Long-test-duration Hypervelocity Detonation-driven Shock Tunnel 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017 作者: Wang Q(汪球); Li JW; Lu P; Li JP(李进平); Zhao W(赵伟); Jiang ZL(姜宗林) 浏览  |  Adobe PDF(679Kb)  |  收藏  |  浏览/下载:386/68  |  提交时间:2018/01/16 Calibration Detonation Heat Transfer Nozzles Spacecraft Supersonic Aerodynamics Thermodynamics Uncertainty Analysis |
| Performance of a detonation driven shock tunnel 会议论文 21st AIAA International Space Planes and Hypersonics Technologies Conference, Xiamen, China, 6-9 March 2017 作者: Li JW; Wang Q(汪球); Zhao W(赵伟); Lu P; Tan YX 浏览  |  Adobe PDF(468Kb)  |  收藏  |  浏览/下载:295/82  |  提交时间:2018/01/16 Detonation Gas Dynamics Hypersonic Flow Shock Tubes Supersonic Aerodynamics |