Effects of row trench holes geometries on an endwall cooling
Gas turbine industries try to extend the gas turbine engine performance. By using the well-known Bryton cycle, the combustor outlet temperature must be increased to have higher efficiencies. However, the turbine inlet temperature increment creates harsh environment for the downstream components of t...
Saved in:
Main Authors: | Che Sidik, N. A., Kianpour, E. |
---|---|
Format: | Article |
Published: |
Penerbit Akademia Baru
2019
|
Subjects: | |
Online Access: | http://eprints.utm.my/id/eprint/92616/ |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
A comparison of cylindrical and row trenched film-cooling holes on a combustor endwall surface at high blowing ratio
by: Kianpour, E., et al.
Published: (2017) -
A detailed study of row-trenched holes at the combustor exit on film-cooling effectiveness
by: Kianpour, E., et al.
Published: (2019) -
A detailed study of effects of row trenched holes at the combustor exit on film cooling effectiveness
by: Kianpour, Ehsan, et al.
Published: (2017) -
Computational investigation of film cooling from cylindrical and row trenched cooling holes near the combustor end wall
by: Kianpour, Ehsan, et al.
Published: (2014) -
The effect of blowing ratio on film cooling effectiveness using cylindrical and row trenched cooling holes with alignment angle of 90 degrees
by: Che Sidik, Nor Azwadi, et al.
Published: (2014)