Aerodynamic analysis for hybrid electric distributed propulsion aircraft

Pan, Tianyi (2020) Aerodynamic analysis for hybrid electric distributed propulsion aircraft. PhD thesis, University of Leeds.

Abstract

Metadata

Keywords: Distributed propulsion, aerodynamic improvement study, engine-wing integration, CFD
Awarding institution: University of Leeds
Academic Units: The University of Leeds > Faculty of Engineering (Leeds) > School of Mechanical Engineering (Leeds) > Institute of Engineering Thermofluids, Surfaces & Interfaces (iETSI) (Leeds)
Identification Number/EthosID (e.g. uk.bl.ethos.123456): uk.bl.ethos.816890
Depositing User: Dr Tianyi Pan
Date Deposited: 04 Nov 2020 16:05
Last Modified: 25 Mar 2021 16:46

Download

Final eThesis - complete (pdf)

Filename: PhD Thesis_Tianyi Pan.pdf

Description: PDF copy of PhD Thesis

Licence: Creative Commons Licence
This work is licensed under a Creative Commons Attribution NonCommercial ShareAlike 4.0 International License

Share / Export

Statistics


You do not need to contact us to get a copy of this thesis. Please use the 'Download' link(s) above to get a copy.
You can contact us about this thesis. If you need to make a general enquiry, please see the Contact us page.