Использование программного комплекса FlowER-U для численного исследования пространственной структуры потока во входном устройстве газотурбинного двигателя
DOI:
https://doi.org/10.15587/1729-4061.2009.20278Keywords:
input device, running part, gasturbine setting, three-dimensional viscid flow, numeral design, calculation netAbstract
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
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