Abstract
A methodology focusing on the evaluation of noise and emission specific direct operating cost components for future aircraft concepts is presented and applied to compare a geared turbofan versus an open rotor powered single-aisle aircraft. High uncertainties in the future development of airline environmental regulations, restrictions and charges complicate the noise and emission related evaluation of new aircraft. The implementation concept is based on the combination of classical procedures for economic aircraft evaluation with scenario techniques.
Full Text 
Sign-in/Register to access full text options
Sign-in/Register to access full text options 
Published version (
Free)
Free) 
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Schedule a call
