05 - Propulsion
INVESTIGATION ON AERO-PROPULSIVE BALANCE FOR HIGH-SPEED POWERED EXPERIMENTAL FLIGHT TEST VEHICLE WITHIN THE HEXAFLY-INT PROJECT
A.A. Gubanov¹, D.S. Ivanyushkin¹, N.V. Kukshinov², A.N. Prokhorov², V.A. Talyzin¹, N.V. Voevodenko¹; ¹Central Aerohydrodynamic Institute named after Professor N.E. Zh, Russia ;²Central Institute of Aviation Motors named after P.I. Baranov, Russia
CFD and experimental research on external aerodynamics, intake performance, and hydrogen-fueled scramjet engine thrust performance for experimental flight test vehicle EFTV of HEXAFLY-NT project are provided. The obtained results made it possible to assess the aero-propulsive balance.