Gorielova K. Hydrodynamic processes in the spacecraft tanks with net mesh delimeters in an variable field of mass forces.

The object are the hydrodynamic processes in the spacecraft tanks with mesh delimiters in an variable field of mass forces. The goal is to establishment of regularities of interaction of liquid flow with the mesh type ensuring means of the liquid continuity and developing on the basis of the obtained regularities of evidence-based methods of calculation of design parameters of these funds. The methods of mathematical and physical simulation, methods of experiment planning, standard methods for the measurement results processing. In the work the physical and mathematical simulation of hydrodynamic processes were carried out in the spacecraft tanks in an alternating field of mass forces; the results allow in normal gravity to conduct pilot testing of the ensuring means of the liquid continuity and to establish patterns of interaction of free surface flow with mesh delimiters. Developed engineering technique allows to optimize the size of the cells net phase separators, to reduce material costs and reduce the time of design process of means to ensure the fuel continuity for prospective spacecraft. Application spheres are machine and instrument-making industries, training courses.