31th Congress of the International Council of the Aeronautical Sciences

05 - Propulsion

COMPLEX NUMERICAL AND EXPERIMENTAL RESEARCH OF HEXAFLY-INT HIGH-SPEED CIVIL AICRAFT MODEL

V.Y. Aleksandrov¹, S.N. Batura¹, O.V. Gouskov¹, N.V. Kukshinov¹, A.N. Prokhorov¹, A.V. Rudinsky¹; ¹Central Institute of Aviation Motors named after P.I. Baranov , Russia

Conducted numerical and experimental research of HEXAFLY-INT aircraft model allowed to validate available methods for high-speed reacting flow calculations. In the work critical factors affected on scramjet operability were determined. Combustion chamber regimes provided positive aeropropulsive balance of model in flight were chosen.


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