33th Congress of the International Council of the Aeronautical Sciences

01.1 - Aircraft Design and Integrated System (Basics and Theory)

SIZING AND OPTIMIZATION OF A MORE ELECTRIC AIRCRAFT INTEGRATING SHORT-TERM INCREMENTAL TECHNOLOGIES

T. Planès¹, S. Delbecq¹, V. Pommier-Budinger¹, V. Palanque¹, E. Bénard¹; ¹ISAE-SUPAERO, France

This paper focuses on the sizing and optimization of a short-medium range aircraft architecture incorporating technological improvements available by 2030. FAST-OAD, an open source framework for overall aircraft design is used to size the architecture. Different optimizations are achieved and a life cycle assessment module is used to analyze the environmental performance of the aircraft.


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