Mathematical simulation and numerical experiment for determining the parameters of heat and mass transfer of thermal vibrational convective flow in the fuel tank of LRM
A numerical study of the structure as averaging and pulsatile flow in the fuel tank of liquid rocket motor (LRM) for exothermic and endothermic reverse combustion processes. The mechanisms of transformation of the structure of flow depending on the orientation of the vectors of gravity and vibration fields. The analysis of the degree of influence of the control parameters and control of non-isothermal processes convective LRM combustion products in the distribution of heat and mass characteristics in varying magnitude and direction of the force fields in low gravity. Numerical estimates are obtained for the distribution of kinetic energy of the averaged and pulsating motion of the convective system.