Thesis icon

Thesis

Thermal modelling and control of high pressure turbine subsystems

Abstract:

The control and monitoring of aircraft engine subsystems is one of the leading fields of research for improving overall performance. As engine sophistication increases, more sensor information becomes available to the digital control system, as well as options for active flow control technologies. It is important to develop control systems that can take full advantage of these developments. For instance, active control of the turbine casing can reduce excess rotor blade tip clearance; for ...

Expand abstract

Actions


Authors


More by this author
Department:
St Catherine’s College, Engineering Science, University of Oxford

Contributors

Department:
University of Oxford
Role:
Supervisor
Department:
University of Oxford
Role:
Supervisor
More from this funder
Funding agency for:
Project
Type of award:
DPhil
Level of award:
Doctoral
Awarding institution:
University of Oxford

Terms of use


Metrics



If you are the owner of this record, you can report an update to it here: Report update to this record

TO TOP