Thesis icon

Thesis

Film cooling of turbine blade trailing edges

Abstract:

In modern gas turbine engines, film cooling is extensively used to cool the components exposed to the hot mainstream gas path. In implementing film cooling on modern gas turbine engines, the trailing edge film poses a particularly challenging design problem. From an aerodynamic point of view, the trailing edge of a blade is designed to be as thin as possible. However, this conflicts with the implementation of the cooling design. The most common method of film cooling the trailing edge is v...

Expand abstract

Actions


Access Document


Files:

Authors


Contributors

Role:
Supervisor
Role:
Supervisor
Role:
Supervisor
Institution:
University of Oxford
Department:
Mathematical,Physical & Life Sciences Division - Engineering Science
More from this funder
Funding agency for:
Janendra C. Telisinghe
Publication date:
2013
Type of award:
DPhil
Level of award:
Doctoral
URN:
uuid:86c06246-16e9-4378-9a61-e09317d31a92
Local pid:
ora:9783

Terms of use


Metrics


Views and Downloads






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

TO TOP