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Flame Dynamics in the Combustion Chamber of Hybrid Rocket Using Multiangle Chemiluminescence 期刊论文
JOURNAL OF PROPULSION AND POWER, 2023
作者:  Luo JX(罗家枭);  Zhang ZL(张泽林);  Lin X(林鑫);  Wang ZZ(王泽众);  Wu K(吴坤);  Zhou GX(周功喜);  Zhang SH(张森豪);  Li F(李飞);  Yu XL(余西龙);  Wu, Jie
Adobe PDF(732Kb)  |  收藏  |  浏览/下载：45/0  |  提交时间：2023/04/20
Combustion Instability  Rayleigh Scattering  Precombustion Chamber  Hybrid Propellant Rocket  Hybrid Rocket Motor  Mass Flow Rate  Convective Heat Transfer  Characteristic Velocity  Planar Laser Induced Fluorescence  Propulsion and Power  
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：269/47  |  提交时间：2021/11/01
Hybrid rocket engine  Fuel mass flow rate  Tunable diode laser absorption spectroscopy  Temperature  Partial pressure  
Experimental investigation of cavity-based scramjet model 会议论文
14th AIAA/AHI International Space Planes and Hypersonics Systems Technologies Conference, Canberra, Australia, November 6, 2006 - November 9, 2006
作者:  Gu HB(顾洪斌);  Chen LH(陈立红);  张新宇(Chang XY)
浏览  |  Adobe PDF(162Kb)  |  收藏  |  浏览/下载：157/70  |  提交时间：2017/06/01
Kerosene Fuel  Mass Flow Rate  Scramjet Engine  
Flow rate analyses and calibrations of kerosene cracking for supersonic combustion 会议论文
41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Tucson, AZ, United states, July 10, 2005 - July 13, 2005
作者:  Fan XJ(范学军);  Yu G(俞刚);  Li JG(李建国)
浏览  |  Adobe PDF(315Kb)  |  收藏  |  浏览/下载：229/60  |  提交时间：2017/06/01
Average Molecular Weight  Chemical Formulae  Cracking Model  Gaseous Products  High Temperature  Ideal Gas Law  Ideal Gas Mixtures  Mass Flow Rate  Mole Fraction  Residence Time  Room Temperature  Sonic Nozzle  Supercritical Condition  Supersonic Combustion  Temperature Dependencies  Thermal Cracking  Three-component