Back to results

University of Illinois at Urbana-Champaign

CHEETA aircraft sizing, performance, and sensitivity

Abstract

dc:description

This thesis presents an overview of the Center for High-Efficiency Electrical Technologies for Aircraft (CHEETA) aircraft design process. The goal of the center was to evaluate liquid hydrogen technology on an electric aircraft concept that utilized liquid hydrogen fuel cells to electrify flight with zero greenhouse gas emissions at the vehicle level. Doing so informs the organization what technologies must be developed to accomplish the goal of zero-emission aviation by 2050. To do so, various estimation methods for weight, aerodynamics, fuel cells, propulsors, and performance are documented. These estimation methods are integrated to a combined performance-sizing methodology. This script uses the estimates produced to create a series of carpet plots that demonstrate the impact of fuel cell size, heat exchanger area, and wing aspect ratio and area to the maximum take-off weight and fuel consumption of the CHEETA aircraft. These carpet plots are used to observe the sensitivity of the system as well as make design decisions for solid oxide and proton exchange membrane fuel cells. A ducted heat exchanger concept that utilizes waste heat to produce thrust was also incorporated and its contributions to the aircraft configuration are presented. The impact of fuel cell degradation to the lifetime performance of the aircraft was also studied, and a strategy for mitigating the performance loss is presented. The combination of all these effects is shown on a payload-range diagram, comparing the aircraft performance to a representative contemporary, incumbent, hydrocarbon-fuelled aircraft.

Degree

thesis:*
Name thesis:degree_name
M.S.
Level thesis:degree_level
Thesis
Discipline thesis:degree_discipline
Aerospace Engineering
Grantor
University of Illinois at Urbana-Champaign
Year dc:date
2022

Author and committee

dc:creator, dc:contributor.*
Author dc:creator
  • Waddington, Elias
Contributors dc:contributor
  • Merret, Jason M

Subjects

dc:subject × 9

Rights

dc:rights
Statement dc:rights
  • Copyright 2022 Elias Waddington
Language dc:language
en, eng

Identifiers

dc:identifier.*
Handle dc:identifier
https://hdl.handle.net/2142/117727

Chain of custody

source
Harvested from
University of Illinois - Urbana-Champaign
Base URL
www.ideals.illinois.edu/oai-pmh
Last updated
2026-07-22
Source record
OAI-PMH GetRecord
citation

Waddington, Elias. CHEETA aircraft sizing, performance, and sensitivity. Thesis thesis, University of Illinois at Urbana-Champaign, 2022. https://hdl.handle.net/2142/117727