26th Congress of International Council of the Aeronautical Sciences
including the 8th AIAA Aviation Technology, Integration, and Operations (ATIO) Conference
14 - 19 September 2008, Anchorage, Alaska, USA
Paper ICAS 2008-2.7.2 INVITED

AERODYNAMIC DESIGN OF THE A400M HIGH-LIFT SYSTEM

D. Reckzeh
AIRBUS, Germany

Keywords: Aerodynamic Design, High-Lift, Propeller, Fixed Vane Flap

The aerodynamic design task for high-lift system for the Airbus A400M Aircraft is presented. Key contents are the multidisciplinary design process in context to the overall aircraft requirements and its specific aerodynamic challenges, as well as the approach for CFD & windtunnel verification.

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