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A comparison of the environmental impact of turboprop and turbofan-powered aircraft

Ugur Kilic (Department of Avionics, Erzincan Binali Yildirim University, Erzincan, Turkey)

Aircraft Engineering and Aerospace Technology

ISSN: 0002-2667

Article publication date: 29 March 2023

Issue publication date: 1 June 2023

229

Abstract

Purpose

This study aims to examine turboprop- and turbofan-powered aircraft, with the same seating capacity flying on the same route and trajectory, and investigate their environmental effects.

Design/methodology/approach

The integrated aircraft noise and emissions modeling platform developed by EUROCONTROL is used for the calculation of fuel burn, CO2, H2O and other gas emissions (NOx, SOx, CO, HC, soot and other trace compounds) for the per phase of flight.

Findings

The striking findings are that turboprop-powered aircraft offer lower required thrust, fuel consumption and total emissions for a short-haul flight, but turbofan-powered aircraft have lower particulate matter, CO and HC emissions than turboprop-powered aircraft. This study suggests that turboprop-powered aircraft are superior to turbofan-powered aircraft in terms of environmental impact for a short-haul flight.

Practical implications

The current research conducts comprehensively fuel consumption and amounts of emissions aspects of turboprop- and turbofan-powered aircraft for sustainable development of airlines by a versatile simulation approach and sheds light on airlines intending to create fleets.

Originality/value

The research offers a systematic aircraft selection for investigators, scientists, airline operators, policy analysts and legislators, by a comprehensive computer simulation method that acknowledges consistently the fuel consumption and detailed emissions analysis of turboprop- and turbofan-powered aircraft.

Keywords

Acknowledgements

The author would like to thank EUROCONTROL for the IMPACT.

Citation

Kilic, U. (2023), "A comparison of the environmental impact of turboprop and turbofan-powered aircraft", Aircraft Engineering and Aerospace Technology, Vol. 95 No. 7, pp. 1092-1098. https://doi.org/10.1108/AEAT-10-2022-0296

Publisher

:

Emerald Publishing Limited

Copyright © 2023, Emerald Publishing Limited

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