𝔖 Bobbio Scriptorium
✦   LIBER   ✦

Experimental investigation on heat transfer characteristics of film cooling using parallel-inlet holes

✍ Scribed by Weihua Yang; Xue Liu; Guohui Li; Jingzhou Zhang

Book ID
116568982
Publisher
Elsevier Science
Year
2012
Tongue
French
Weight
838 KB
Volume
60
Category
Article
ISSN
1290-0729

No coin nor oath required. For personal study only.

πŸ“œ SIMILAR VOLUMES

Effects of film cooling hole shape on he
Effects of film cooling hole shape on heat transfer
✍ Zhu Huiren; Xu Duchun; Guo Tao; Liu Songling πŸ“‚ Article πŸ“… 2004 πŸ› John Wiley and Sons 🌐 English βš– 663 KB

## Abstract The effects of hole shapes, secondary injection Reynolds numbers, and blowing ratios on the heat transfer downstream of film cooling holes have been investigated by using a large‐scale low‐speed loop wind tunnel. The test model consists of five film cooling holes. Experiments on dustpan

The interior heat transfer characteristi
The interior heat transfer characteristics of gas turbine blade due to sparse film cooling holes
✍ Zhang Jingyu; Chang Haiping πŸ“‚ Article πŸ“… 2005 πŸ› John Wiley and Sons 🌐 English βš– 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