the mixed fuel of n -decane and toluene) for kerosene(Jet A-1) were chosen
and detailed reaction mechanisms (67 species and 344 reactions for n -decane
118 species and 527 reactions for the mixed fuel of n -decane and 1
2
4-trimethylbenzene
and 84 species and 440 reactions for the mixed fuel of n -decane and toluene) for the ignition and combustion of these three surrogate fuels were analyzed.The ignition characteristics and the premixed combustion processes of these three surrogate fuels in the shock tube and the perfectly stirred reactor were simulated especially
and the simulation results were compared with the experimental data.Furthermore
the effect of volume percentage of two species in the mixed fuel on the ignition and premixed combustion characteristics were analyzed.The results show that these two mixed fuels represent the ignition and combustion characteristics of Jet A-1 more accurately than n -decane single fuel does.At the same time
the effect of volume percentage of two species in the mixed fuel on the ignition and premixed combustion characteristics are remarkable.
Faculty of Aerospace Engineering, Shenyang Aerospace University
School of Energy and Power Engineering, Xi'an Jiaotong University
Jiangsu Province Key Laboratory of Aerospace Power System, College of Energy and Power Engineering, Nanjing University of Aeronautics and Astronautics
National Key Laboratory of Science and Technology on Aero-Engine Aero-thermodynamics, School of Energy and Power Engineering, Beijing University of Aeronautics and Astronautics
College of Power and Energy Engineering, Shenyang Aerospace University