Transonic Fan Design for a Separated Intake at High Angle of Attack
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Repository DOI
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Type
Thesis
Change log
Authors
Mohankumar, Benjamin
Abstract
[Restricted]
Description
Date
2021-04-30
Advisors
Hall, Cesare
Keywords
aerodynamics, turbomachinery, gas turbine, aerospace, aviation, engineering, design
Qualification
Doctor of Philosophy (PhD)
Awarding Institution
University of Cambridge
Rights
Sponsorship
Technology Strategy Board (113075)
Rolls-Royce plc.