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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Isfahan University of Technology
2020-01-01
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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 |
work_keys_str_mv |
AT tprabu optimizationofwrapangleinthemixedflowimpellerforreducingflowlosses AT pviswanathan optimizationofwrapangleinthemixedflowimpellerforreducingflowlosses AT ngokulkannan optimizationofwrapangleinthemixedflowimpellerforreducingflowlosses AT rrudramoorthy optimizationofwrapangleinthemixedflowimpellerforreducingflowlosses AT afirthouse optimizationofwrapangleinthemixedflowimpellerforreducingflowlosses |
_version_ |
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