Numerical study of test gas vitiation effects on hydrogen-fueled scramjet combustion  

作　　者：CHEN Chao-qun TIAN Liang XU Xu 

机构地区：[1]School of Astronautics,Beijing University of Aeronautics and Astronautics,Beijing 100191,China

出　　处：《航空动力学报》2012年第2期326-334,共9页Journal of Aerospace Power

摘　　要：The effects of major vitiated species(H2O and CO2) and minor vitiated species(H,OH and O radicals) produced by combustion air preheater on ignition and combustion of hydrogen-fueled scramjet were numerically investigated.Firstly,kinetic analyses with CHEMKIN SENKIN code were conducted to evaluate the effects of contamination on the ignition delay times of hydrogen fuel over a range of temperature and pressure variations.Then numerical simulation of a three-dimensional reacting flow in hydrogen-fueled scramjet combustor was performed.The two-equation shear stress transport κ-ω turbulence model was used for modeling turbulence and 33 reactions finite-rate chemistry was used for modeling the H2/air kinetics.The results show that: free radical species such as H,O,and OH may significantly promote the ignition process of hydrogen-air at relatively low initial temperature and pressure.However,H2O and CO2 have inhibition effects on the ignition process.Under the same conditions,H2O has more effective inhibition effects than CO2.The temperature and pressure rise due to combustion are lower in the air vitiated with H2O and CO2 because of their higher heat capacities and more dissociation.Combustion efficiency and thrust calculated for vitiated air case are lower than clean air case.These results indicate the importance of accounting for vitiation effects when extrapolating performance data from ground test to flight demonstration.The effects of major vitiated species （H2O and CO2） and minor vitiated species （H,OH and O radicals） produced by combustion air preheater on ignition and combustion of hydrogen-fueled seramjet were numerically investigated. Firstly, kinetic analyses with CHEMKIN SENKIN code were conducted to evaluate the effects of contamination on the ignition delay times of hydrogen fuel over a range of temperature and pressure variations. Then numerical simulation of a three-dimensional reacting flow in hydrogen-fueled seramjet combustor was performed. The two-equation shear stress transport k-ω turbulence model was used for modeling turbulence and 33 reactions finite-rate chemistry was used for modeling the H2/air kinetics. The results show that： free radical species such as H,O,and OH may significantly promote the ignition process of hydrogen-air at relatively low initial temperature and pressure. However, H2O and CO2 have inhibition effects on the ignition process. Under the same conditions, H2O has more effective inhibition effects than CO2. The temperature and pressure rise due to combustion are lower in the air vitiated with H2O and CO2 because of their higher heat capacities and more dissociation. Combustion efficiency and thrust calculated for vitiated air case are lower than clean air case. These results indicate the importance of accounting for vitiation effects when extrapolating performance data from ground test to flight demonstration.

关 键 词：SCRAMJET CONTAMINANT IGNITION supersonic combustion PREHEATER 

分 类 号：V434[航空宇航科学与技术—航空宇航推进理论与工程]