An Investigation on the Effect of Endwall Movement on the Tip Clearance Loss Using Annular Turbine Cascade

The aerodynamic losses in gas turbines are mainly caused by profile loss secondary flow, and tip leakage loss. This study focuses on tip leakage flow of high-pressure turbine stages. An annular turbine cascade was constructed with fixed blades on the casing, and the distance between blade tip and th...

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Main Authors: Hesham M. El-Batsh, Magdy Bassily Hanna
Format: Article
Language:English
Published: Wiley 2011-01-01
Series:International Journal of Rotating Machinery
Online Access:http://dx.doi.org/10.1155/2011/489150
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author Hesham M. El-Batsh
Magdy Bassily Hanna
author_facet Hesham M. El-Batsh
Magdy Bassily Hanna
author_sort Hesham M. El-Batsh
collection DOAJ
description The aerodynamic losses in gas turbines are mainly caused by profile loss secondary flow, and tip leakage loss. This study focuses on tip leakage flow of high-pressure turbine stages. An annular turbine cascade was constructed with fixed blades on the casing, and the distance between blade tip and the hub was considered as tip clearance gap. The effect of endwall movement on loss mechanism was investigated by using experimental and numerical techniques. The measurements were obtained while the hub was fixed but the numerical calculations were carried out for both stationary and moving cascades. Upstream and downstream flows were measured by using a calibrated five-hole pressure probe. The steady incompressible turbulent flow was obtained by solving Reynolds averaged Navier-Stokes equations and by employing shear stress transport (SST) k-ω turbulence model. The total pressure loss coefficient obtained from the numerical technique was compared with the experimental measurements, and the comparison showed good agreement. Tip clearance vortices were observed in the tip clearance gap. It was found through this study that end-wall movement reduces tip leakage loss through the cascade.
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institution Kabale University
issn 1023-621X
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language English
publishDate 2011-01-01
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record_format Article
series International Journal of Rotating Machinery
spelling doaj-art-cc3d6da0915d45ce94c54617129e01a42025-02-03T05:51:34ZengWileyInternational Journal of Rotating Machinery1023-621X1542-30342011-01-01201110.1155/2011/489150489150An Investigation on the Effect of Endwall Movement on the Tip Clearance Loss Using Annular Turbine CascadeHesham M. El-Batsh0Magdy Bassily Hanna1Mechanical Engineering Department, High Institute of Technology, Benha University, Benha 13512, EgyptMechanical Power Engineering and Energy Department, Faculty of Engineering, Minia University, Minia, EgyptThe aerodynamic losses in gas turbines are mainly caused by profile loss secondary flow, and tip leakage loss. This study focuses on tip leakage flow of high-pressure turbine stages. An annular turbine cascade was constructed with fixed blades on the casing, and the distance between blade tip and the hub was considered as tip clearance gap. The effect of endwall movement on loss mechanism was investigated by using experimental and numerical techniques. The measurements were obtained while the hub was fixed but the numerical calculations were carried out for both stationary and moving cascades. Upstream and downstream flows were measured by using a calibrated five-hole pressure probe. The steady incompressible turbulent flow was obtained by solving Reynolds averaged Navier-Stokes equations and by employing shear stress transport (SST) k-ω turbulence model. The total pressure loss coefficient obtained from the numerical technique was compared with the experimental measurements, and the comparison showed good agreement. Tip clearance vortices were observed in the tip clearance gap. It was found through this study that end-wall movement reduces tip leakage loss through the cascade.http://dx.doi.org/10.1155/2011/489150
spellingShingle Hesham M. El-Batsh
Magdy Bassily Hanna
An Investigation on the Effect of Endwall Movement on the Tip Clearance Loss Using Annular Turbine Cascade
International Journal of Rotating Machinery
title An Investigation on the Effect of Endwall Movement on the Tip Clearance Loss Using Annular Turbine Cascade
title_full An Investigation on the Effect of Endwall Movement on the Tip Clearance Loss Using Annular Turbine Cascade
title_fullStr An Investigation on the Effect of Endwall Movement on the Tip Clearance Loss Using Annular Turbine Cascade
title_full_unstemmed An Investigation on the Effect of Endwall Movement on the Tip Clearance Loss Using Annular Turbine Cascade
title_short An Investigation on the Effect of Endwall Movement on the Tip Clearance Loss Using Annular Turbine Cascade
title_sort investigation on the effect of endwall movement on the tip clearance loss using annular turbine cascade
url http://dx.doi.org/10.1155/2011/489150
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