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50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition
This work introduces the work conducted in the EU JTI project ANOLOCO, which has aimed at an assessment of aerodynamic and aeroacoustic performance of several high-lift configurations of a regional aircraft. The high-lift designs are for a laminar and slat-less wing, including configurations with a double slotted flap, single slotted flap, drooped nose and a Krueger flap. The aerodynamic performance is assessed from steady state RANS calculations up to maximum lift. The aeroacoustic performancedoi:10.2514/6.2012-277 fatcat:n5vmnqrclbe7dcl33tmhtx4hnm