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An interactive boundary layer method for subsonic aerofoil flows
File(s)
Author(s)
Ho, Pui Yin
Type
Thesis
Version
Open Access
Date Issued
1989
Date Awarded
1989
URI
Copyright Statement
Attribution NoDerivatives 4.0 International Licence (CC BY-ND)
License URL
Creator
Ho, Pui Yin
Publisher Department
Department of Mechanical Engineering
Publisher Institution
Imperial College London
Qualification Level
Doctoral
Qualification Name
PhD