Boundary-layer transition in relation to turbomachinery blades



Abu-Ghannam, Bishara Jeries
(1979) Boundary-layer transition in relation to turbomachinery blades. PhD thesis, University of Liverpool.

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Item Type: Thesis (PhD)
Uncontrolled Keywords: Engineering
Depositing User: Symplectic Admin
Date Deposited: 20 Jan 2023 11:11
Last Modified: 20 Jan 2023 13:38
DOI: 10.17638/03167204
Copyright Statement: Copyright © and Moral Rights for this thesis and any accompanying data (where applicable) are retained by the author and/or other copyright owners. A copy can be downloaded for personal non-commercial research or study, without prior permission or charge.
Digitisation Notes : Unnumbered page before no.i Unnumbered page before no.A1
URI: https://livrepository.liverpool.ac.uk/id/eprint/3167204