33th Congress of the International Council of the Aeronautical Sciences

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

PROPELLER AIRCRAFT DESIGN OPTIMIZATION FOR CLIMATE IMPACT REDUCTION

R. Thijssen¹, P. Proesmans¹, R. Vos¹; ¹Delft University of Technology, Netherlands

This paper yields insight into the climate impact reduction of propeller-powered aircraft. CO2 and non-CO2 climate effects and operating costs are considered in a multidisciplinary design optimisation. A comparison with turbofan counterparts shows that climate-optimal, propeller aircraft can outperform turbofan aircraft in the medium-range category. This is relevant for future design studies.


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