Journal article icon

Journal article

Heat transfer measurements to a gas turbine cooling passage with inclined ribs

Abstract:

The local heat transfer coefficient distribution over all four walls of a large-scale model of a gas turbine cooling passage have been measured in great detail. A new method of determining the heat transfer coefficient to the rib surface has been developed and the contribution of the rib, at 5 percent blockage, to the overall roughened heat transfer coefficient was found to be considerable. The vortex-dominated flow field was interpreted from the detailed form of the measured local heat trans...

Expand abstract

Actions


Authors


More by this author
Institution:
University of Oxford
Division:
MPLS
Department:
Engineering Science
Role:
Author
Journal:
Journal of Turbomachinery
Volume:
120
Issue:
1
Pages:
63-69
Publication date:
1998-01-01
ISSN:
0889-504X
Source identifiers:
399309
Language:
English
Pubs id:
pubs:399309
UUID:
uuid:2b12a5b9-07c6-4d34-ae6b-96983b1d3a6b
Local pid:
pubs:399309
Deposit date:
2013-11-17

Terms of use


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