Optimization of Wrap Angle in the Mixed Flow Impeller for Reducing Flow Losses

In this paper, mixed flow impeller is investigated to reduce the secondary flow loss and attain uniform flow at impeller exit by changing the wrap angle in the trailing edge (called as stacking condition). The 3D inverse design methodology is adopted for the blade profile generation using ADT Turbo...

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Main Authors: T. Prabu, P. Viswanathan, N. Gokul Kannan, R. Rudramoorthy, A. Firthouse
Format: Article
Language:English
Published: Isfahan University of Technology 2020-01-01
Series:Journal of Applied Fluid Mechanics
Subjects:
Online Access:http://jafmonline.net/JournalArchive/download?file_ID=54282&issue_ID=1009
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spelling doaj-4536540ffc6c45048a0895881721cde72020-11-25T03:22:01ZengIsfahan University of Technology Journal of Applied Fluid Mechanics1735-35722020-01-0113619491957.Optimization of Wrap Angle in the Mixed Flow Impeller for Reducing Flow LossesT. Prabu0P. Viswanathan1N. Gokul Kannan2R. Rudramoorthy3A. Firthouse4PSG College of Technology, Coimbatore, Tamil Nadu, 641004, IndiaPSG College of Technology, Coimbatore, Tamil Nadu, 641004, IndiaPSG College of Technology, Coimbatore, Tamil Nadu, 641004, IndiaPSG College of Technology, Coimbatore, Tamil Nadu, 641004, IndiaPSG College of Technology, Coimbatore, Tamil Nadu, 641004, IndiaIn this paper, mixed flow impeller is investigated to reduce the secondary flow loss and attain uniform flow at impeller exit by changing the wrap angle in the trailing edge (called as stacking condition). The 3D inverse design methodology is adopted for the blade profile generation using ADT Turbo suite software. The internal flow analysis of the base design is evaluated using commercial computational fluid dynamics (CFD). A single stage proto type model is tested and the experimental results have strong agreement with numerical analysis results. Further the impeller is designed with different wrap angle at the trailing edge of the hub and shroud region. The pump performance curve is obtained from numerical analysis for the optimized impellers from the ADT Turbo suite and compared with the base design. The wrap angle between 8 ̊ - 15̊ degree in hub region has the less secondary flow losses compared to the stacking in the shroud region. Higher wrap angle above 17 ̊ degree increases the diffusion ratio which in turn induces non-uniform flow at the impeller exit and also increases instability.http://jafmonline.net/JournalArchive/download?file_ID=54282&issue_ID=1009trailing edge; inverse design; computational fluid dynamics; wrap angle.
collection DOAJ
language English
format Article
sources DOAJ
author T. Prabu
P. Viswanathan
N. Gokul Kannan
R. Rudramoorthy
A. Firthouse
spellingShingle T. Prabu
P. Viswanathan
N. Gokul Kannan
R. Rudramoorthy
A. Firthouse
Optimization of Wrap Angle in the Mixed Flow Impeller for Reducing Flow Losses
Journal of Applied Fluid Mechanics
trailing edge; inverse design; computational fluid dynamics; wrap angle.
author_facet T. Prabu
P. Viswanathan
N. Gokul Kannan
R. Rudramoorthy
A. Firthouse
author_sort T. Prabu
title Optimization of Wrap Angle in the Mixed Flow Impeller for Reducing Flow Losses
title_short Optimization of Wrap Angle in the Mixed Flow Impeller for Reducing Flow Losses
title_full Optimization of Wrap Angle in the Mixed Flow Impeller for Reducing Flow Losses
title_fullStr Optimization of Wrap Angle in the Mixed Flow Impeller for Reducing Flow Losses
title_full_unstemmed Optimization of Wrap Angle in the Mixed Flow Impeller for Reducing Flow Losses
title_sort optimization of wrap angle in the mixed flow impeller for reducing flow losses
publisher Isfahan University of Technology
series Journal of Applied Fluid Mechanics
issn 1735-3572
publishDate 2020-01-01
description In this paper, mixed flow impeller is investigated to reduce the secondary flow loss and attain uniform flow at impeller exit by changing the wrap angle in the trailing edge (called as stacking condition). The 3D inverse design methodology is adopted for the blade profile generation using ADT Turbo suite software. The internal flow analysis of the base design is evaluated using commercial computational fluid dynamics (CFD). A single stage proto type model is tested and the experimental results have strong agreement with numerical analysis results. Further the impeller is designed with different wrap angle at the trailing edge of the hub and shroud region. The pump performance curve is obtained from numerical analysis for the optimized impellers from the ADT Turbo suite and compared with the base design. The wrap angle between 8 ̊ - 15̊ degree in hub region has the less secondary flow losses compared to the stacking in the shroud region. Higher wrap angle above 17 ̊ degree increases the diffusion ratio which in turn induces non-uniform flow at the impeller exit and also increases instability.
topic trailing edge; inverse design; computational fluid dynamics; wrap angle.
url http://jafmonline.net/JournalArchive/download?file_ID=54282&issue_ID=1009
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AT ngokulkannan optimizationofwrapangleinthemixedflowimpellerforreducingflowlosses
AT rrudramoorthy optimizationofwrapangleinthemixedflowimpellerforreducingflowlosses
AT afirthouse optimizationofwrapangleinthemixedflowimpellerforreducingflowlosses
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