Reaction kinetic numerical simulation of combustion process and emission formation in aero-engine combustor
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Reaction kinetic numerical simulation of combustion process and emission formation in aero-engine combustor
Vol. 28, Issue 2, (2013)
作者机构:
1. 大连理工大学 能源与动力工程学院,辽宁,大连,116024
2. 沈阳航空航天大学 航空航天工程学院,沈阳,110136
作者简介:
基金信息:
DOI:
CLC:
Published:2013
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MA Hong-an, XIE Mao-zhao, ZENG Wen, et al. Reaction kinetic numerical simulation of combustion process and emission formation in aero-engine combustor[J]. 2013, 28(2).
DOI:
MA Hong-an, XIE Mao-zhao, ZENG Wen, et al. Reaction kinetic numerical simulation of combustion process and emission formation in aero-engine combustor[J]. 2013, 28(2).DOI:
Reaction kinetic numerical simulation of combustion process and emission formation in aero-engine combustor
A detailed mechanism and a reduced reaction mechanism (including 50 species and 118 reactions) of n-decane which was chosen as a surrogate fuel for kerosene were built.The ignition delay time of this surrogate fuel in the shock tube and the process of premixed combustion in the premixed burner were simulated by adopting the detailed and reduced reaction mechanisms
and the simulated results were compared with the experimental data.Furthermore
the flow characteristics and the reaction kinetic characteristics of combustion process and the formation of emissions and active species in a tube of the annular tube combustor were analyzed by combining this reduced reaction mechanism with the CFD computational software(Fluent)
and the computational results were compared with that of the global reaction mechanism of C12H23 fuel.The results show that the ignition delay time
the shape of the profiles of the mole fractions of the reactants
the major combustion products simulated using the reduced mechanism agree well with the experimental data.Furthermore
compared with the global reaction mechanism of C12H23 fuel
when adopting the reduced reaction mechanism of n- decane
temperature field accords well with the practical situation
and the computational outlet temperature is closer to the design outlet temperature of the combustor.At the same time
the process of fuel low temperature decomposition and formations of pyrolysis products
active species and main emissions are better detailedly understood.
Simulation method of short crack propagation in turbine disks based on crystal plasticity
Numerical simulation of internal flow field in gas generator of fire extinguishing bomb
Numerical simulation of light-craft effects onlaser supported donation wave with gas-liquid two phase propellant
Low-Reynolds-number wake flows of a triangular prism
Influence of combustor shape on self-ignition in solid fuel scramjet
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