32th Congress of the International Council of the Aeronautical Sciences

01 - Aircraft Design and Integrated Systems

INTEGRATION OF FUSELAGE-MOUNTED OVER-WING ENGINES ON A MID-RANGE AIRCRAFT

P. Wegener, DLR - German Aerospace Center, Germany

In order to enable the integration of UHBR engines in a commercial aircraft configuration, configurations with engines located above the wing were optimized using RANS CFD methods as part of the AVACON project. Positive installation effects due to the integration between the wing and the engine nacelle could be demonstrated.rn


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