物理化学学报Issue(4)：636-642,7.DOI:10.3866/PKU.WHXB201501231
RP-3航空煤油替代燃料及其化学反应动力学模型
RP-3 Aviation Kerosene Surrogate Fuel and the Chemical Reaction Kinetic Model
摘要
Abstract
A four-component RP-3 aviation kerosene surrogate fuel, comprising 40% n-decane/42% n-dodecane/13%ethycyclohexane/5%p-xylene (molar fraction), was presented. Experiments showed the physical and chemical similarity of the surrogate fuel to the real RP-3. Counterflow, twin-flame experiments were used to determine the laminar flame speeds of both the real and the surrogate fuel and showed that the surrogate fuel accurately modeled the burning rate of real RP-3. A semi-detailed chemical reaction mechanism for ignition and oxidation of the RP-3 surrogate fuel that consists of 168 species and 1089 elementary reactions has been developed. Experimental results validate the model and highlight its ability to accurately predict the ignition delay times and laminar flame speeds of real RP-3.关键词
RP-3航空煤油/替代燃烧/反应机理/火焰传播速度/对冲火焰Key words
RP-3 aviation kerosene/Surrogate fuel/Reaction mechanism/Laminar flame speed/Counter-flow flame分类
化学化工引用本文复制引用
郑东,于维铭,钟北京..RP-3航空煤油替代燃料及其化学反应动力学模型[J].物理化学学报,2015,(4):636-642,7.基金项目
The project was supported by the National Natural Science Foundation of China (91441113).国家自然科学基金(91441113)资助项目 （91441113）
