一种喷气燃料替代物的动力学分析及用于计算流体动力学应用的骨架机构的发展

Nurina Sharmin, Efstathios-Al. Tingas
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引用次数: 4

摘要

摘要研究了适用于jet a -1和RP-3航空燃料的三组份替代喷气燃料(66.2%正十二烷,15.8%正丙苯,18.0% 1,3,5-三甲基环己烷)的自燃动力学。
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Dynamics Analysis of a Jet-Fuel Surrogate and Development of a Skeletal Mechanism for Computational Fluid Dynamic Applications
AbstractThe autoignition dynamics of a three-component surrogate jet fuel (66.2% n-dodecane, 15.8% n-proplylbenzene, 18.0% 1,3,5-trimethylcyclohexane) suitable for usage as Jet A-1 and RP-3 aviatio...
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