๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

The effect of turbulence intensity on film cooling of gas turbine blade from trenched shaped holes

โœ Scribed by S. Baheri Islami, B. A. Jubran


Book ID
113023676
Publisher
Springer-Verlag
Year
2011
Tongue
English
Weight
764 KB
Volume
48
Category
Article
ISSN
1432-1181

No coin nor oath required. For personal study only.


๐Ÿ“œ SIMILAR VOLUMES


Simulation of fabrication for gas turbin
โœ M.H. Wang; D. Zhu ๐Ÿ“‚ Article ๐Ÿ“… 2009 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 565 KB

Electrochemical machining (ECM) is an important manufacture technology in machining difficult-to-cut materials without tool wear and residual stress. In this study, ECM is used to machine the turbulated cooling hole on gas turbine blade for enhance efficiency of aircraft engine. However, because of

The interior heat transfer characteristi
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