Regenerative cooling
utilizing on-board endothermic hydrocarbon
fuels of the high-temperature components of the scramjet engine plays
a paramount role in maintaining the reliability and durability of
the systems. A molecular kinetic model was proposed by modifying the
Kumar–Kunzru kinetic model to describe the thermal cracking
of n-decane at supercritical pressures. The apparent
kinetic parameters at different pressures were optimized by the Levenberg–Marquardt
algorithm. After the model validation, the role of pressure on the
chemical heat absorption rate during n-decane pyrolysis
was investigated using the one-dimensional plug flow model. It was
found that the heat absorption rate first increases and then slightly
decreases as the temperature increases at all pressures. The highest
chemical heat absorption rate is located at a conversion of 41.81%,
53.34%, and 59.40% at 3, 4, and 5 MPa. In addition, the effect of
pressure on n-decane pyrolysis was quantitated using
the equivalence temperature. Under the simulation conditions considered
in the present study, each 1 MPa increase in pressure produced the
same conversion as a temperature decrease of 6.5–10 K. Finally,
in order to extrapolate the kinetic model to a wider range of pressure
conditions, a model extrapolation method based on the activation volume
was proposed.