Design and sizing eVTOL aircraft (theoretical portion)

The emergence of the electric Vertical Takeoff and Landing (eVTOL) industry has presented a potential solution to the worsening problem of traffic congestion. However, majority of fixed-wing eVTOL aircraft are still in their preliminary design stages. There is a need to have a simplified tool to rap...

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Main Author: Koh, Andy Jun Hoong
Other Authors: James Wang Ming
Format: Final Year Project
Language:English
Published: Nanyang Technological University 2022
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Online Access:https://hdl.handle.net/10356/159254
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Institution: Nanyang Technological University
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spelling sg-ntu-dr.10356-1592542023-03-04T20:17:21Z Design and sizing eVTOL aircraft (theoretical portion) Koh, Andy Jun Hoong James Wang Ming School of Mechanical and Aerospace Engineering james.wang@ntu.edu.sg Engineering::Aeronautical engineering The emergence of the electric Vertical Takeoff and Landing (eVTOL) industry has presented a potential solution to the worsening problem of traffic congestion. However, majority of fixed-wing eVTOL aircraft are still in their preliminary design stages. There is a need to have a simplified tool to rapidly evaluate these different conceptual eVTOL configurations with limited inputs. This report introduces the EVTOL Performance Analysis Tool, known as ePERF. ePERF is a MATLAB-based analysis developed specifically for evaluating the performance of various fixed-wing eVTOL configurations in their preliminary design phases. A detailed documentation of the methodology behind the three main modules in ePERF has been provided. They include a rotary wing module based on momentum theory, a drag estimation module for forward flight based on component level drag build-up method, and an energy module for range calculation. ePERF was first successfully validated against the performance data of two top viable eVTOLs in the market. It was then used to evaluate three different example eVTOL configurations: lift + cruise, tiltrotor, and fixed lift + tiltrotor. The results show that the tiltrotor configuration, which had the lowest weight, had the best performance. It was concluded that reducing eVTOL weight is the key factor in improving performance. Bachelor of Engineering (Aerospace Engineering) 2022-06-11T13:14:51Z 2022-06-11T13:14:51Z 2022 Final Year Project (FYP) Koh, A. J. H. (2022). Design and sizing eVTOL aircraft (theoretical portion). Final Year Project (FYP), Nanyang Technological University, Singapore. https://hdl.handle.net/10356/159254 https://hdl.handle.net/10356/159254 en B350 application/pdf Nanyang Technological University
institution Nanyang Technological University
building NTU Library
continent Asia
country Singapore
Singapore
content_provider NTU Library
collection DR-NTU
language English
topic Engineering::Aeronautical engineering
spellingShingle Engineering::Aeronautical engineering
Koh, Andy Jun Hoong
Design and sizing eVTOL aircraft (theoretical portion)
description The emergence of the electric Vertical Takeoff and Landing (eVTOL) industry has presented a potential solution to the worsening problem of traffic congestion. However, majority of fixed-wing eVTOL aircraft are still in their preliminary design stages. There is a need to have a simplified tool to rapidly evaluate these different conceptual eVTOL configurations with limited inputs. This report introduces the EVTOL Performance Analysis Tool, known as ePERF. ePERF is a MATLAB-based analysis developed specifically for evaluating the performance of various fixed-wing eVTOL configurations in their preliminary design phases. A detailed documentation of the methodology behind the three main modules in ePERF has been provided. They include a rotary wing module based on momentum theory, a drag estimation module for forward flight based on component level drag build-up method, and an energy module for range calculation. ePERF was first successfully validated against the performance data of two top viable eVTOLs in the market. It was then used to evaluate three different example eVTOL configurations: lift + cruise, tiltrotor, and fixed lift + tiltrotor. The results show that the tiltrotor configuration, which had the lowest weight, had the best performance. It was concluded that reducing eVTOL weight is the key factor in improving performance.
author2 James Wang Ming
author_facet James Wang Ming
Koh, Andy Jun Hoong
format Final Year Project
author Koh, Andy Jun Hoong
author_sort Koh, Andy Jun Hoong
title Design and sizing eVTOL aircraft (theoretical portion)
title_short Design and sizing eVTOL aircraft (theoretical portion)
title_full Design and sizing eVTOL aircraft (theoretical portion)
title_fullStr Design and sizing eVTOL aircraft (theoretical portion)
title_full_unstemmed Design and sizing eVTOL aircraft (theoretical portion)
title_sort design and sizing evtol aircraft (theoretical portion)
publisher Nanyang Technological University
publishDate 2022
url https://hdl.handle.net/10356/159254
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