𝔖 Bobbio Scriptorium
✦   LIBER   ✦

Numerical study on film cooling effectiveness from shaped and crescent holes

✍ Scribed by Ping Dai; Feng Lin

Book ID
105925364
Publisher
Springer-Verlag
Year
2010
Tongue
English
Weight
582 KB
Volume
47
Category
Article
ISSN
1432-1181

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

Film cooling from two rows of holes with
Film cooling from two rows of holes with opposite orientation angles: injectant behavior and adiabatic film cooling effectiveness
✍ Joon Ahn; In Sung Jung; Joon Sik Lee πŸ“‚ Article πŸ“… 2003 πŸ› Elsevier Science 🌐 English βš– 450 KB

The present paper is aiming at describing the injectant behaviors from two rows of film cooling holes with opposite orientation angles. Boundary layer temperature distributions were measured in the streamwise normal plane to illustrate the interaction between the injectant from the holes in the upst