Numerical investigation of rectangular twisted hole on film cooling for gas turbine blades
This paper investigates a new method of film cooling using swirling coolant flow through a rectangular twisted film cooling holes with spirally corrugated tube. Two different air flows with different in temperatures were used in this study. Throughout the investigation, blowing ratio was varied from...
Saved in:
Main Authors: | , , , |
---|---|
Format: | Conference or Workshop Item |
Language: | English |
Published: |
2014
|
Subjects: | |
Online Access: | http://eprints.utm.my/id/eprint/60902/1/Aminuddinsaat2014_NumericalInvestigationofRectangularTwistedHole.pdf http://eprints.utm.my/id/eprint/60902/ |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Be the first to leave a comment!