An urgent requirement for high-precision numerical simulation
of
modern aero-engines is the development of a highly simplified and
accurate reaction mechanism for aviation kerosene. However, there
is still lack of a reduced mechanism that can effectively capture
the low- and high-temperature characteristics of RP-3 aviation kerosene.
In light of this, in this study, a novel methodology for developing
skeletal mechanism by combining the detailed C0–C4 mechanism and C5–C
n
high-carbon molecular skeletal mechanism was proposed and applied.
To construct the RP-3 skeletal mechanism, a surrogate fuel consisting
of 54% n-dodecane, 22% 2,5-dimethylhexane, 14% 1,3,5-trimethylbenzene,
and 10% decalin was utilized. Based on the proposed methodology, a
skeletal mechanism comprising 153 species and 858 reactions has been
developed. Various combustion characteristics of each surrogate component
and the RP-3 aviation kerosene, such as the ignition delay, concentration
of material components, laminar flame, and NO emission, were examined
to validate the developed mechanism. The proposed methodology in this
study offers a novel approach to develop mechanisms for high-carbon
fuels. Additionally, the developed skeletal mechanism serves as a
foundation for the design and optimization of aero-engines.