04.1 - Aerospace Grade Materials, Structural Analysis, Fatigue and Damage Tolerance
CONCEPTUAL DESIGN AND TOPOLOGY OPTIMIZATION OF A COMPLIANT MORPHING FLAP FOR NEXT GENERATION HYBRID-ELECTRIC REGIONAL AIRCRAFT
M.C. Noviello¹, I. Dimino¹, S. Ameduri¹, A. Concilio¹; ¹The Italian Aerospace Research Centre (CIRA), Italy
CONCEPTUAL DESIGN AND TOPOLOGY OPTIMIZATION OF A COMPLIANT MORPHING FLAP FOR NEXT GENERATION HYBRID-ELECTRIC REGIONAL AIRCRAFT