Использование программного комплекса FlowER-U для численного исследования пространственной структуры потока во входном устройстве газотурбинного двигателя

Results of numerical research of spatial current in the input device of the gas turbine engine with the design GTR&PC”Zorya-Mashproekt” are presented. The researches were made with the help of program complex FlowER-U. The directions of aerodynamic perfection of similar devices are also presented