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Massachusetts Institute of Technology

Influence of Turbofan Engine Design Parameters on Aircraft Environmental Impact

Abstract

dc:description.abstract

Despite the emergence of new energy carriers and propulsion systems architectures, turbofan engines power the majority of commercial aircraft. Therefore, aviation’s environmental impacts are significantly influenced by the design of these turbofan engines. Hence, we should drive the design of modern turbofan engines, informed with each design parameter’s effect on environmental implications, namely the climate and air quality impacts. To understand the connection between the engine design parameters and an aircraft’s environmental impact, it is important to have the capability to quantify the environmental impact resulting from a combined “Aircraft-Engine- Operation” scenario. Through modeling and connecting aircraft, engines, flight operations, emissions, and their resulting impacts on climate and air quality, we can link the end-to-end impact propagation chain and evaluate the outcomes of any engine design alteration. We investigate free design variables such as overall pressure ratio (OPR), fan pressure ratio (FPR), and turbine entry temperature (TET), as well as technology level indicators such as component efficiencies, cooling, and material temperature capability. Sensitivities are calculated for three different reference engines, and the differences in trends between the engines are analyzed. Influence of external-to-aviation uncertainties and valuation choices are also illustrated. Comparison between Jet-A and different sustainable aviation fuels (SAFs) are conducted from an environmental and societal point of view. The study also explores how the derived influence coefficients or sensitivities can provide valuable guidance to stakeholders when making decisions regarding technological investments, design space change, or regulatory assessments.

Degree

thesis:*
Name thesis:degree_name
Master
Department dc:contributor.department
Massachusetts Institute of Technology. Department of Aeronautics and Astronautics
Grantor dc:publisher
Massachusetts Institute of Technology
Year dc:date.issued
2023

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Lee, Kanghyun
Advisors dc:contributor.advisor
  • Barrett, Steven R. H.
  • Speth, Raymond L.

Rights

dc:rights
Statement dc:rights
  • In Copyright - Educational Use Permitted
  • Copyright retained by author(s)

Identifiers

dc:identifier.*
Handle dc:identifier.uri
https://hdl.handle.net/1721.1/151448
OAI identifier oai:identifier
oai:dspace.mit.edu:1721.1/151448

Chain of custody

source
Harvested from
MIT
Base URL
dspace.mit.edu/oai/request
Last updated
2026-07-22
Source record
OAI-PMH GetRecord
related terms
citation

Lee, Kanghyun. Influence of Turbofan Engine Design Parameters on Aircraft Environmental Impact. Massachusetts Institute of Technology, 2023. https://hdl.handle.net/1721.1/151448