A simulation of film cooling in the leading edge region of a turbine blade (trench effect on film effectiveness from cylinder in crossflow)
Film cooling is one of the cooling system techniques applied to the turbine blade. Gas turbine use film cooling technique to protect turbine blade from expose directly to a hot gas to avoid the blade from defect. The focus of this investigation is to investigate the effect of embedded three diffe...
Saved in:
Main Author: | Pairan, Mohamad Rasidi |
---|---|
Format: | Thesis |
Language: | English English |
Published: |
2012
|
Subjects: | |
Online Access: | http://eprints.uthm.edu.my/1943/1/24p%20MOHAMAD%20RASIDI%20PAIRAN.pdf http://eprints.uthm.edu.my/1943/2/MOHAMAD%20RASIDI%20PAIRAN%20WATERMARK.pdf http://eprints.uthm.edu.my/1943/ |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Experimental And Numerical Analysis On The Cooling Performance Of Synthetic Jet At Low Reynolds Number
by: Ho, Roger Zhen Yu
Published: (2018) -
Classification of damage severity in natural fibre composites using principal component analysis
by: Mohamad, Zaleha, et al.
Published: (2018) -
Evaluation of a suitable material
for soft actuator through
experiments and FE Simulations
by: Muhammad Razif, Muhammad Rusyd, et al.
Published: (2020) -
Kesan latihan pliometriks Shuttle MVP ke atas peningkatan kuasa bahagian bawah badan atlet novis lompat kijang
by: Frankie, Lumpil
Published: (2015) -
Molecular Mechanics Simulations Of Quartz Etching Process
by: Manap, Abdul Haadi Abdul
Published: (2016)