Analysis of factors determining numerical solution in the calculation of flow with combustion using the ONERA experimental model
W. Liu
Moscow Institute of Physics and Technology NRU, Dolgoprudny, Russia
Keywords: supersonic flow, combustion, channel, roughness, kinetic mechanism
Abstract
Three-dimensional numerical simulation of a transverse hydrogen jet blowing into a duct with a supersonic flow of air (warmed by a fire heater) has been carried out. The study is based on experimental data obtained at the ONERA-LAERTE facility. The RANS equations for the reacting gas were solved, closed by the SST model and various kinetic mechanisms of hydrogen combustion in air. The channel walls roughness was taken into account. The dependence of the flow characteristics on such physical factors as the shape of the fuel injector channel, the effective roughness height, and various methods of describing molecular diffusion has been studied. It has been established that the equivalent diameter of a grain of sand has a significant influence on the longitudinal pressure distribution in the duct. The influence of chemical kinetics on the flow structure in separation zones within the duct is demonstrated.
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