An investigation into full-ring radial-gap air-riding seals for aeroengines

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An investigation into full-ring radial-gap air-riding seals for aeroengines

This thesis focuses on a study carried out for modelling, designing and testing a full-ring radial-gap air-riding seal configuration for applications in a Gas Turbine Engine. On reviewing the open literature in the field of air riding seals, it was realised that the majority of existing seal desi...

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Bibliographic Details
Main Author:	Kumar, Shubham
Format:	Thesis (University of Nottingham only)
Language:	English
Published:	2019
Subjects:	Seals (Closures); Aircraft gas-turbines
Online Access:	https://eprints.nottingham.ac.uk/59365/

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