34th Congress of the International Council of the Aeronautical Sciences

04.2 - Aerostructures Design, Structural Dynamics, Aeroelasticity

STRUCTURAL DESIGN OF NEXT-GENERATION REGIONAL GREEN AIRCRAFT

L. Pustina¹, F. Mastroddi¹, P. Della Vecchia, University of Naples “Federico II”, Italy; G. Cerino, LEONARDO, Aircraft Division, Italy; ¹Sapienza University of Rome, Italy

This paper presents a novel approach for designing next-generation green aircraft, focusing on structural optimization. It employs a simplified FEM to minimize structural weight while maintaining structural integrity for several aircraft configurations, including those with unconventional powertrain architectures.


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