Effect of Secondary Flows on Heat Transfer of a Gas Turbine Blade
This study presents experimental and numerical investigation for three-dimensional heat transfer characteristics in a turbine blade. An experimental setup was installed with a turbine cascade of five-blade channels. Blade heat transfer measurements were performed for the middle channel under uniform...
Saved in:
Main Authors: | Hesham M. El-Batsh, Sameh A. Nada, Samia Nasreldin Abdo, Abdelgalil A. El-Tayesh |
---|---|
Format: | Article |
Language: | English |
Published: |
Wiley
2013-01-01
|
Series: | International Journal of Rotating Machinery |
Online Access: | http://dx.doi.org/10.1155/2013/797841 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Similar Items
-
Effect of the Radial Pressure Gradient on the Secondary Flow Generated in an Annular Turbine Cascade
by: Hesham M. El-Batsh
Published: (2012-01-01) -
Conjugate heat transfer in wedged latticework cooling ducts with ejection flow for turbine blades
by: Binye Yu, et al.
Published: (2025-01-01) -
Local Mass and Heat Transfer on a Turbine Blade Tip
by: P. Jin, et al.
Published: (2003-01-01) -
Theoretical Analysis of Heat Transfer Through an Idealized Gas Turbine Blade Model with Thermal Barrier Coating
by: Orhan Aydin, et al.
Published: (2002-01-01) -
Blade Deterioration in a Gas Turbine Engine
by: W. Tabakoff, et al.
Published: (1998-01-01)