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....
Saved in:
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
-
Simulation and experimental study of double holes film cooling
by: Aminnuddin, Mohd Hazim Fadli
Published: (2017) -
Investigation of film cooling effectiveness from cylindrical
cooling hole with anti vortex generator by numerical
simulation
by: Abu Zarida, Abdallah Ali
Published: (2015) -
Combustion characteristics of a spark ignition engine operating with liquid lpg injection
by: Mustaffa, Norrizal
Published: (2019) -
Performance and emissions of compression ignition engine fueled with preheated blend of vegetable oil
by: Suffian, Mohamad Mokhsen
Published: (2014) -
Gas turbine performence based creep life estimation using soft computing technique
by: Mohamed Zarti, Almehdi
Published: (2012)