Numerical and Experimental Study of the Blade Profile of a Savonius Type Rotor Implementing a Multi-Blade Geometry

In the present study, the implementation of multi-blade profiles in a Savonius rotor was evaluated in order to increase the pressure in the blade’s intrados and, thus, decrease motion resistance. The geometric proportions of the secondary element were determined, which maximized the rotor’s performa...

Descripción completa

Guardado en:
Detalles Bibliográficos
Autores principales: Luis A. Gallo, Edwin L. Chica, Elkin G. Flórez, Felipe A. Obando
Formato: article
Lenguaje:EN
Publicado: MDPI AG 2021
Materias:
CFD
T
Acceso en línea:https://doaj.org/article/76ff798fdda04a368645393937f57a2d
Etiquetas: Agregar Etiqueta
Sin Etiquetas, Sea el primero en etiquetar este registro!
id oai:doaj.org-article:76ff798fdda04a368645393937f57a2d
record_format dspace
spelling oai:doaj.org-article:76ff798fdda04a368645393937f57a2d2021-11-25T16:31:58ZNumerical and Experimental Study of the Blade Profile of a Savonius Type Rotor Implementing a Multi-Blade Geometry10.3390/app1122105802076-3417https://doaj.org/article/76ff798fdda04a368645393937f57a2d2021-11-01T00:00:00Zhttps://www.mdpi.com/2076-3417/11/22/10580https://doaj.org/toc/2076-3417In the present study, the implementation of multi-blade profiles in a Savonius rotor was evaluated in order to increase the pressure in the blade’s intrados and, thus, decrease motion resistance. The geometric proportions of the secondary element were determined, which maximized the rotor’s performance. For this, the response surface methodology was used through a full factorial experimental design and a face-centered central composite design, consisting of three factors, each with three levels. The response variable that was sought to be maximized was the power coefficient (<inline-formula><math xmlns="http://www.w3.org/1998/Math/MathML" display="inline"><semantics><msub><mi>C</mi><mi>P</mi></msub></semantics></math></inline-formula>), which was obtained through the numerical simulation of the geometric configurations resulting from the different treatments. All geometries were studied under the same parameters and computational fluid dynamics models through the <i>ANSYS Fluent</i> software. The results obtained through both experimental designs showed a difference of only 1.06% in the performance estimates using the regression model and 3.41% when simulating the optimal proportions geometries. The optimized geometry was characterized by a <inline-formula><math xmlns="http://www.w3.org/1998/Math/MathML" display="inline"><semantics><msub><mi>C</mi><mi>P</mi></msub></semantics></math></inline-formula> of 0.2948, which constitutes an increase of 10.8% in its performance compared to the profile without secondary elements and of 51.2% compared to the conventional semicircular profile. The numerical results were contrasted with experimental data obtained using a wind tunnel, revealing a good degree of fit.Luis A. GalloEdwin L. ChicaElkin G. FlórezFelipe A. ObandoMDPI AGarticlewind powerSavonius rotormulti-elementexperimental designresponse surfaceCFDTechnologyTEngineering (General). Civil engineering (General)TA1-2040Biology (General)QH301-705.5PhysicsQC1-999ChemistryQD1-999ENApplied Sciences, Vol 11, Iss 10580, p 10580 (2021)
institution DOAJ
collection DOAJ
language EN
topic wind power
Savonius rotor
multi-element
experimental design
response surface
CFD
Technology
T
Engineering (General). Civil engineering (General)
TA1-2040
Biology (General)
QH301-705.5
Physics
QC1-999
Chemistry
QD1-999
spellingShingle wind power
Savonius rotor
multi-element
experimental design
response surface
CFD
Technology
T
Engineering (General). Civil engineering (General)
TA1-2040
Biology (General)
QH301-705.5
Physics
QC1-999
Chemistry
QD1-999
Luis A. Gallo
Edwin L. Chica
Elkin G. Flórez
Felipe A. Obando
Numerical and Experimental Study of the Blade Profile of a Savonius Type Rotor Implementing a Multi-Blade Geometry
description In the present study, the implementation of multi-blade profiles in a Savonius rotor was evaluated in order to increase the pressure in the blade’s intrados and, thus, decrease motion resistance. The geometric proportions of the secondary element were determined, which maximized the rotor’s performance. For this, the response surface methodology was used through a full factorial experimental design and a face-centered central composite design, consisting of three factors, each with three levels. The response variable that was sought to be maximized was the power coefficient (<inline-formula><math xmlns="http://www.w3.org/1998/Math/MathML" display="inline"><semantics><msub><mi>C</mi><mi>P</mi></msub></semantics></math></inline-formula>), which was obtained through the numerical simulation of the geometric configurations resulting from the different treatments. All geometries were studied under the same parameters and computational fluid dynamics models through the <i>ANSYS Fluent</i> software. The results obtained through both experimental designs showed a difference of only 1.06% in the performance estimates using the regression model and 3.41% when simulating the optimal proportions geometries. The optimized geometry was characterized by a <inline-formula><math xmlns="http://www.w3.org/1998/Math/MathML" display="inline"><semantics><msub><mi>C</mi><mi>P</mi></msub></semantics></math></inline-formula> of 0.2948, which constitutes an increase of 10.8% in its performance compared to the profile without secondary elements and of 51.2% compared to the conventional semicircular profile. The numerical results were contrasted with experimental data obtained using a wind tunnel, revealing a good degree of fit.
format article
author Luis A. Gallo
Edwin L. Chica
Elkin G. Flórez
Felipe A. Obando
author_facet Luis A. Gallo
Edwin L. Chica
Elkin G. Flórez
Felipe A. Obando
author_sort Luis A. Gallo
title Numerical and Experimental Study of the Blade Profile of a Savonius Type Rotor Implementing a Multi-Blade Geometry
title_short Numerical and Experimental Study of the Blade Profile of a Savonius Type Rotor Implementing a Multi-Blade Geometry
title_full Numerical and Experimental Study of the Blade Profile of a Savonius Type Rotor Implementing a Multi-Blade Geometry
title_fullStr Numerical and Experimental Study of the Blade Profile of a Savonius Type Rotor Implementing a Multi-Blade Geometry
title_full_unstemmed Numerical and Experimental Study of the Blade Profile of a Savonius Type Rotor Implementing a Multi-Blade Geometry
title_sort numerical and experimental study of the blade profile of a savonius type rotor implementing a multi-blade geometry
publisher MDPI AG
publishDate 2021
url https://doaj.org/article/76ff798fdda04a368645393937f57a2d
work_keys_str_mv AT luisagallo numericalandexperimentalstudyofthebladeprofileofasavoniustyperotorimplementingamultibladegeometry
AT edwinlchica numericalandexperimentalstudyofthebladeprofileofasavoniustyperotorimplementingamultibladegeometry
AT elkingflorez numericalandexperimentalstudyofthebladeprofileofasavoniustyperotorimplementingamultibladegeometry
AT felipeaobando numericalandexperimentalstudyofthebladeprofileofasavoniustyperotorimplementingamultibladegeometry
_version_ 1718413144847548416