Film cooling effectiveness in a gas turbine engine: a review
This study was carried out to extend database knowledge about the function of film cooling holes at the end of combustor and the inlet of turbine. Using the well-known Brayton cycle, raising the turbine inlet temperature is the key to obtain higher engine efficiency in gas turbine engines. However,...
Saved in:
| Main Authors: | , , |
|---|---|
| Format: | Article |
| Language: | English |
| Published: |
Penerbit UTM
2014
|
| Subjects: | |
| Online Access: | http://eprints.utm.my/id/eprint/52886/1/NorAzwadiChe2014_Filmcoolingeffectiveness.pdf http://eprints.utm.my/id/eprint/52886/ https://dx.doi.org/10.11113/jt.v71.3717 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|