02.4 - Applied Aerodynamics
NUMERICAL AND EXPERIMENTAL INVESTIGATION OF DIFFERENT INTAKE CONFIGURATIONS OF HEXAFLY-INT FACILITY MODULE
V.Y. Aleksandrov¹, M.K. Danilov¹, O.V. Gouskov¹, S.V. Gusev¹, N.V. Kukshinov¹, A.N. Prokhorov¹, V.S. Zakharov¹; ¹CIAM, Russia
The results of numerical and experimental investigation of HEXAFLY-INT facility module intake are given. Technological intake configuration was proposed for manufacturing simplification. Numerical and experimental results demonstrated the robustness of intake, its stable work in the wide range of free-stream parameters and angles of attack.