01.2 - Aircraft Design and Integrated System (Applications)
IMPACT OF WELL-TO-TANK EFFICIENCY AND EMISSIONS ON HYBRID AIRCRAFT DESIGN OPTIMIZATION
M. Blandino¹, M.M. Molinari¹, J. Liberatori¹, P.P. Ciottoli¹, R. Malpica Galassi¹; ¹Sapienza Università di Roma, Italy
We present a general framework for the design of sustainable hybrid aircraft which pursues minimal renewable energy consumption and CO2 emissions, taking into account the complete well-to-wake energy route. The design methodology is applied on a hybrid SAF/electric regional aircraft. Polynomial Chaos Expansion is employed to efficiently build stochastic optimal designs.