Journal article icon

Journal article

USE OF AN IMMERSED MESH FOR HIGH RESOLUTION MODELLING OF FILM COOLING FLOWS

Abstract:

The development of a high pressure turbine requires the accurate prediction of flow within and around film cooling holes. However the length scales inherent to film cooling flows produce a large disparity against those of themainstreamflow, hence they can not be resolved by a mesh generated for an aerodynamics analysis. Furthermore, the process of meshing cooling holes is not only time consuming but cumbersome; thus making the parametric study of film cooling effectiveness for a given blade g...

Expand abstract
Publication status:
Published

Actions


Access Document


Publisher copy:
10.1115/GT2011-45354

Authors


More by this author
Institution:
University of Oxford
Department:
Oxford, MPLS, Engineering Science
Journal:
PROCEEDINGS OF THE ASME TURBO EXPO 2011, VOL 5, PTS A AND B
Volume:
5
Issue:
PARTS A AND B
Pages:
159-170
Publication date:
2012
DOI:
URN:
uuid:7144bf79-0a51-4abb-9a05-9160d6b188de
Source identifiers:
351382
Local pid:
pubs:351382
Language:
English

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