Study of aerodynamic parameters of air distributors during interaction of round non-coaxial jets

Purpose of reseach. The aim of the work is to determine the parameters of the resulting flow in the interaction of counter-misaligned air flows to ensure an intensive decrease in air velocity in production and technological premises of small volume. To achieve this goal, it is necessary to solve such tasks as analyzing existing theoretical provisions and methods for calculating air distribution systems for small production and technological premises; development of a mathematical model of the process of interaction of oncoming incompatible flows and to determine the parameters of the resulting air flow depending on the geometric characteristics of the device. The object of the study is the supply ventilation systems in industrial and technological premises of small volume with insignificant thermal loads. The subject of the study is the processes of formation of the resulting air flow created by the interaction of countermisaligned air flows. Methods. Methods of mathematical modeling of air flow motion based on the equations of aerodynamics. Results. The aerodynamic characteristics of the resulting jet are obtained – the Boussinesq coefficient and the velocity field coefficient. Conclusion. In the ambiguities, between two-meter-long-range extravehicular jets and two-meter-long-range converging streams in the inner regions, a spatial vortex zone is formed with a maximum extravehicular gradient velocity. At the boundary of the jet stream there is an intense interaction with the surrounding air, the vector of the propeller is directed by the opposite direction, and the quantity of the speed of the plane depends on the speed of the jet, which changes the nature of the swirling movements. The results show that the actual level of overshoot during a load surge is determined in the first approximation by the increment value multiplied by the difference in the values of thermal conductivity, winding-oil at the initial and final temperatures of the oils in the channels of the cooled windings, and this difference itself depends on the magnitude of the incremental damage. Optimal factor intervals for the values of the maximum value of the functions are obtained: t – from 40 to 120; ρ – from 800 to 900; c – from 1.4 to 2.3.