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Recent Advances in the Study of Film Cooling on the Gas Turbine Blade

โœ Scribed by Dai, Ping; Li, Shuang Xiu


Book ID
126796137
Publisher
Trans Tech Publications, Ltd.
Year
2014
Tongue
English
Weight
261 KB
Volume
971-973
Category
Article
ISSN
1662-8958

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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