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Factors influencing heat transfer to the pressure surfaces of gas turbine blades

โœ Scribed by B.W Martin; A Brown

Book ID
107893319
Publisher
Elsevier Science
Year
1979
Tongue
English
Weight
757 KB
Volume
1
Category
Article
ISSN
0142-727X

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๐Ÿ“œ SIMILAR VOLUMES

Calculation of heat transfer rates to ga
Calculation of heat transfer rates to gas turbine blades
โœ L.D. Daniels; W.B. Browne ๐Ÿ“‚ Article ๐Ÿ“… 1981 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 699 KB

Five computer programs are used to calculate heat transfer rates to gas turbine blades and the results compared with experimental work on blade cascades. The programs use different methods to model the turbulence quantities. The experimental work was carried out recently in the University of Oxford

The interior heat transfer characteristi
The interior heat transfer characteristics of gas turbine blade due to sparse film cooling holes
โœ Zhang Jingyu; Chang Haiping ๐Ÿ“‚ Article ๐Ÿ“… 2005 ๐Ÿ› John Wiley and Sons ๐ŸŒ English โš– 213 KB

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