“…In this study, to calculate the high-temperature oxidation of kerosene and gasoline in a supersonic direct-flow combustion chamber, kinetic models of combustion of the main reference fuels, n-decane and n-heptane, are used, respectively. Combustion of n-decane is described by a reduced kinetic mechanism [18], which includes 68 reactions and 44 components. The mechanism is based on the kinetic model of combustion of n-decane [37], supplemented by the initiating reactions of high-temperature decomposition of n-decane [33].…”