Two-stage optimization process.

<div><p>To enhance the aerodynamic performance of centrifugal impellers, this study presents an advanced optimization design methodology. This methodology addresses the challenges associated with numerous design variables, inflexible configurations, and low optimization efficiency. We pr...

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Main Author: Yesong Wang (331723) (author)
Other Authors: Zixuan Sun (3495020) (author), Jisheng Liu (219678) (author), Manxian Liu (20298265) (author), Yong Zhou (23772) (author)
Published: 2024
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_version_ 1852025043032211456
author Yesong Wang (331723)
author2 Zixuan Sun (3495020)
Jisheng Liu (219678)
Manxian Liu (20298265)
Yong Zhou (23772)
author2_role author
author
author
author
author_facet Yesong Wang (331723)
Zixuan Sun (3495020)
Jisheng Liu (219678)
Manxian Liu (20298265)
Yong Zhou (23772)
author_role author
dc.creator.none.fl_str_mv Yesong Wang (331723)
Zixuan Sun (3495020)
Jisheng Liu (219678)
Manxian Liu (20298265)
Yong Zhou (23772)
dc.date.none.fl_str_mv 2024-11-20T18:38:14Z
dc.identifier.none.fl_str_mv 10.1371/journal.pone.0310792.g010
dc.relation.none.fl_str_mv https://figshare.com/articles/figure/Two-stage_optimization_process_/27870679
dc.rights.none.fl_str_mv CC BY 4.0
info:eu-repo/semantics/openAccess
dc.subject.none.fl_str_mv Biophysics
Medicine
Cell Biology
Neuroscience
Biotechnology
Evolutionary Biology
Computational Biology
Space Science
Biological Sciences not elsewhere classified
Mathematical Sciences not elsewhere classified
rated operating conditions
objective evolutionary algorithms
normal operating conditions
enhancing solution quality
computational fluid dynamics
centrifugal impeller based
centrifugal compressor blades
two parameterization approaches
two optimization stages
optimization results demonstrate
numerous design variables
local mapping model
global mapping model
low optimization efficiency
blade geometry configuration
optimization design
local optimization
blade geometry
centrifugal impellers
parameterization methods
optimization space
isentropic efficiency
enable global
xlink ">
thoroughly explored
surge margin
study presents
methodology addresses
inflexible configurations
form deformation
control bodies
challenges associated
bezier surfaces
bezier surface
aerodynamic performance
dc.title.none.fl_str_mv Two-stage optimization process.
dc.type.none.fl_str_mv Image
Figure
info:eu-repo/semantics/publishedVersion
image
description <div><p>To enhance the aerodynamic performance of centrifugal impellers, this study presents an advanced optimization design methodology. This methodology addresses the challenges associated with numerous design variables, inflexible configurations, and low optimization efficiency. We propose two distinct spline function parameterization techniques: a global mapping model for Bezier surfaces and a local mapping model for Free-Form Deformation (FFD) control bodies. We investigate the impact of these parameterization methods on blade geometry configuration and aerodynamic performance. By integrating these two parameterization approaches with multi-objective evolutionary algorithms and Computational Fluid Dynamics (CFD) techniques, we enable global and local optimization of centrifugal compressor blades. The optimization results demonstrate a 1.77% enhancement in isentropic efficiency under rated operating conditions, a 7.8% increase in surge margin, a 1.6% improvement in isentropic efficiency under normal operating conditions, and an 11.8% enhancement in surge margin. Through two optimization stages, the optimization space for blade geometry is thoroughly explored, enhancing solution quality and contributing to the advancement of impeller mechanical optimization design theory.</p></div>
eu_rights_str_mv openAccess
id Manara_386f2541ffe68e378620e4e5157f6dfd
identifier_str_mv 10.1371/journal.pone.0310792.g010
network_acronym_str Manara
network_name_str ManaraRepo
oai_identifier_str oai:figshare.com:article/27870679
publishDate 2024
repository.mail.fl_str_mv
repository.name.fl_str_mv
repository_id_str
rights_invalid_str_mv CC BY 4.0
spelling Two-stage optimization process.Yesong Wang (331723)Zixuan Sun (3495020)Jisheng Liu (219678)Manxian Liu (20298265)Yong Zhou (23772)BiophysicsMedicineCell BiologyNeuroscienceBiotechnologyEvolutionary BiologyComputational BiologySpace ScienceBiological Sciences not elsewhere classifiedMathematical Sciences not elsewhere classifiedrated operating conditionsobjective evolutionary algorithmsnormal operating conditionsenhancing solution qualitycomputational fluid dynamicscentrifugal impeller basedcentrifugal compressor bladestwo parameterization approachestwo optimization stagesoptimization results demonstratenumerous design variableslocal mapping modelglobal mapping modellow optimization efficiencyblade geometry configurationoptimization designlocal optimizationblade geometrycentrifugal impellersparameterization methodsoptimization spaceisentropic efficiencyenable globalxlink ">thoroughly exploredsurge marginstudy presentsmethodology addressesinflexible configurationsform deformationcontrol bodieschallenges associatedbezier surfacesbezier surfaceaerodynamic performance<div><p>To enhance the aerodynamic performance of centrifugal impellers, this study presents an advanced optimization design methodology. This methodology addresses the challenges associated with numerous design variables, inflexible configurations, and low optimization efficiency. We propose two distinct spline function parameterization techniques: a global mapping model for Bezier surfaces and a local mapping model for Free-Form Deformation (FFD) control bodies. We investigate the impact of these parameterization methods on blade geometry configuration and aerodynamic performance. By integrating these two parameterization approaches with multi-objective evolutionary algorithms and Computational Fluid Dynamics (CFD) techniques, we enable global and local optimization of centrifugal compressor blades. The optimization results demonstrate a 1.77% enhancement in isentropic efficiency under rated operating conditions, a 7.8% increase in surge margin, a 1.6% improvement in isentropic efficiency under normal operating conditions, and an 11.8% enhancement in surge margin. Through two optimization stages, the optimization space for blade geometry is thoroughly explored, enhancing solution quality and contributing to the advancement of impeller mechanical optimization design theory.</p></div>2024-11-20T18:38:14ZImageFigureinfo:eu-repo/semantics/publishedVersionimage10.1371/journal.pone.0310792.g010https://figshare.com/articles/figure/Two-stage_optimization_process_/27870679CC BY 4.0info:eu-repo/semantics/openAccessoai:figshare.com:article/278706792024-11-20T18:38:14Z
spellingShingle Two-stage optimization process.
Yesong Wang (331723)
Biophysics
Medicine
Cell Biology
Neuroscience
Biotechnology
Evolutionary Biology
Computational Biology
Space Science
Biological Sciences not elsewhere classified
Mathematical Sciences not elsewhere classified
rated operating conditions
objective evolutionary algorithms
normal operating conditions
enhancing solution quality
computational fluid dynamics
centrifugal impeller based
centrifugal compressor blades
two parameterization approaches
two optimization stages
optimization results demonstrate
numerous design variables
local mapping model
global mapping model
low optimization efficiency
blade geometry configuration
optimization design
local optimization
blade geometry
centrifugal impellers
parameterization methods
optimization space
isentropic efficiency
enable global
xlink ">
thoroughly explored
surge margin
study presents
methodology addresses
inflexible configurations
form deformation
control bodies
challenges associated
bezier surfaces
bezier surface
aerodynamic performance
status_str publishedVersion
title Two-stage optimization process.
title_full Two-stage optimization process.
title_fullStr Two-stage optimization process.
title_full_unstemmed Two-stage optimization process.
title_short Two-stage optimization process.
title_sort Two-stage optimization process.
topic Biophysics
Medicine
Cell Biology
Neuroscience
Biotechnology
Evolutionary Biology
Computational Biology
Space Science
Biological Sciences not elsewhere classified
Mathematical Sciences not elsewhere classified
rated operating conditions
objective evolutionary algorithms
normal operating conditions
enhancing solution quality
computational fluid dynamics
centrifugal impeller based
centrifugal compressor blades
two parameterization approaches
two optimization stages
optimization results demonstrate
numerous design variables
local mapping model
global mapping model
low optimization efficiency
blade geometry configuration
optimization design
local optimization
blade geometry
centrifugal impellers
parameterization methods
optimization space
isentropic efficiency
enable global
xlink ">
thoroughly explored
surge margin
study presents
methodology addresses
inflexible configurations
form deformation
control bodies
challenges associated
bezier surfaces
bezier surface
aerodynamic performance