Stall and surge in axial flow compressors

The objective of the work described in this thesis is twofold; to elucidate the nature of stall and surge in an axial flow aeroengine compressor, and to improve on current computational stall modelling techniques. Particular attention is paid to the initial stages of the stall/surge transient, and t...

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Bibliographic Details
Main Author: Wilson, Alexander George
Other Authors: Elder, R. L.
Language:en
Published: Cranfield University 2016
Online Access:http://dspace.lib.cranfield.ac.uk/handle/1826/10432