02.4 - Applied Aerodynamics
BOUNDARY LAYER STATE INFLUENCE ON START OF THE INWARD-TURNING INTAKE
N.V. Voevodenko¹, A.A. Gubanov¹, D.Y. Gusev¹, M.A. Ivankin, TsAGi, Russia; D.S. Ivanyushkin¹, V.Y. Lunin¹, P.A. Meshennikov¹, Y.G. Shvalev¹, V.A. Talyzin¹, V.A. Yakovleva¹; ¹TsAGI, Russia
This paper presents numerical and experimental studies (in TsAGI’S wind tunnel T-116) of the flow in the air intake model of the high-speed experimental test vehicle (EFTV) within the HEXAFLY-INT project. The main emphasis is on the boundary layer state influence on the air intake performances.