Experimental and simulation study on the effect of geometrical and flow parameters for combined-hole film cooling

Film cooling method was applied to the turbine blades to provide thermal protection from high turbine inlet temperatures in modern gas turbines. Recent literature discovers that combining two cylindrical holes of film cooling is one of the ways to further enhance the film cooling performances....

Full description

Saved in:
Bibliographic Details
Main Author: Hassan, Haswira
Format: Thesis
Language:English
English
English
Published: 2016
Subjects:
Online Access:http://eprints.uthm.edu.my/751/1/24p%20HASWIRA%20HASSAN.pdf
http://eprints.uthm.edu.my/751/2/HASWIRA%20HASSAN%20COPYRIGHT%20DECLARATION.pdf
http://eprints.uthm.edu.my/751/3/HASWIRA%20HASSAN%20WATERMARK.pdf
Tags: Add Tag
No Tags, Be the first to tag this record!

Similar Items