(National Aviation University, 2018-10) Tereshchenko, Yuriy; Терещенко, Юрій Юрійович; Doroshenko, Katerіna; Дорошенко, Катерина Вікторівна; Lastivka, Ivan; Ластівка, Іван Олексійович; Tereshchenko, Yuriy; Терещенко, Юрій Матвійович
The paper presents the results of numerical simulation of flow in compressor cascades with active flow control at different angles of attack. It is shown that the active control of flow past the blades affects the value of deviation angle of flow behind the blades. The paper analyzes the influence of the effect of supercirculation on the aerodynamic characteristics of compressor cascades with active control of the flow past the blades.
