01 - Aircraft Design and Integrated SystemsINTEGRATION OF FUSELAGE-MOUNTED OVER-WING ENGINES ON A MID-RANGE AIRCRAFTP. 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 |