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机译:HCCI条件下实际燃料的自燃:高压冲击管实验和现象学建模
LAV, Aerothermochemistry and Combustion Systems Laboratory, Institute of Energy Technology, ETH Zuerich, Sonneggstrasse 3, 8092 Zuerich, Switzerland;
IVG, Institute for Combustion and Gasdynamics, University of Duisburg-Essen, Lotharstraße 1, 47057 Duisburg, Germany;
LAV, Aerothermochemistry and Combustion Systems Laboratory, Institute of Energy Technology, ETH Zuerich, Sonneggstrasse 3, 8092 Zuerich, Switzerland;
LAV, Aerothermochemistry and Combustion Systems Laboratory, Institute of Energy Technology, ETH Zuerich, Sonneggstrasse 3, 8092 Zuerich, Switzerland;
IVG, Institute for Combustion and Gasdynamics, University of Duisburg-Essen, Lotharstraße 1, 47057 Duisburg, Germany;
IVG, Institute for Combustion and Gasdynamics, University of Duisburg-Essen, Lotharstraße 1, 47057 Duisburg, Germany;
IVG, Institute for Combustion and Gasdynamics, University of Duisburg-Essen, Lotharstraße 1, 47057 Duisburg, Germany;
LAV, Aerothermochemistry and Combustion Systems Laboratory, Institute of Energy Technology, ETH Zuerich, Sonneggstrasse 3, 8092 Zuerich, Switzerland;
arrhenius model; ignition delay time; practical fuels; HCCI conditions; kinetic modeling;
机译:异十六烷在高温至中温和高压下的自燃:冲击管实验和动力学建模
机译:喷气燃料的点火延迟时间:冲击管在广泛条件下的实验和替代模型的预测
机译:甲苯掺杂正庚烷和异辛烷/空气混合物的自燃:高压激波管实验和动力学建模
机译:冲击管内线性不饱和喷气燃料化合物自燃延迟时间的测量
机译:在实际条件下,在点火延迟时间之前和期间进行冲击管流场的数值模拟。
机译:单脉冲冲击管实验和动力学建模直接煤液化衍生燃料热解的研究它与传统的RP-3喷气燃料混合
机译:对双燃料HCCI发动机中的燃烧进行建模。使用建模和仿真研究天然气和柴油均质充量压缩点火(HCCI)发动机的爆震,压缩比,当量比和正时。