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Infrared thermography as applied to film cooling of gas turbine components

โœ Scribed by Schulz, A


Book ID
120307519
Publisher
Institute of Physics
Year
2000
Tongue
English
Weight
524 KB
Volume
11
Category
Article
ISSN
0957-0233

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The film cooling technique is one of the most useful cooling methods. At present, the midchord region of gas turbine blades in an aeroengine often adopt a sparse film cooling technique and impingement cooling technique at the same time. So the interior heat transfer characteristics on the inner side