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.