Computational Design of an Energy-Efficient Small Axial-Flow Fan Using Staggered Blades with Winglets

dc.contributor.author Mustafa Tutar
dc.contributor.author Janset Betul Cam
dc.date JAN 9
dc.date.accessioned 2025-10-06T16:20:59Z
dc.date.issued 2025
dc.description.abstract The present study introduces a conceptual design of a small axial-flow fan. Both individual and combined effects of blade stagger angle and winglet on the performance of the fan design are investigated in design and off-design operating conditions using a computational flow methodology. A stepwise solution in which a proper stagger angle adjustment of a specifically generated blade profile is followed by appending a winglet at the tip of the blade with consideration of different geometrical parameters is proposed to improve the performance characteristics of the fan. The initial model comparison analysis demonstrates that a three-dimensional Reynolds-averaged Navier-Stokes (RANS) equation-based renormalization group (RNG) k-epsilon turbulence modeling approach coupled with the multiple reference frame (MRF) technique which adapts multi-block topology generation meshing method successfully resolves the rotating flow around the fan. The results suggest that the use of a proper stagger angle with the winglet considerably increases the fan performance and the fan attains the best total efficiency with an additional stagger angle of +10 degrees and a winglet which has a curvature radius of 6.77 mm and a twist angle of -7 degrees for the investigated dimensioning range. The present study also underlines the effectiveness of passive flow control mechanisms of the stagger angle and winglets for energy-efficient axial-flow fans.
dc.identifier.doi 10.3390/ijtpp10010001
dc.identifier.issn 2504-186X
dc.identifier.uri http://dx.doi.org/10.3390/ijtpp10010001
dc.identifier.uri https://gcris.yasar.edu.tr/handle/123456789/6638
dc.language.iso English
dc.publisher MDPI
dc.relation.ispartof International Journal of Turbomachinery, Propulsion and Power
dc.source INTERNATIONAL JOURNAL OF TURBOMACHINERY PROPULSION AND POWER
dc.subject small axial-flow fan, aerodynamic performance, energy efficiency, flow control, computational fluid dynamics (CFD), multiple reference frame (MRF)
dc.subject AERODYNAMIC PERFORMANCE, NUMERICAL-SIMULATION, NOISE
dc.title Computational Design of an Energy-Efficient Small Axial-Flow Fan Using Staggered Blades with Winglets
dc.type Article
dspace.entity.type Publication
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gdc.bip.influenceclass C5
gdc.bip.popularityclass C4
gdc.coar.type text::journal::journal article
gdc.collaboration.industrial false
gdc.description.startpage 1
gdc.description.volume 10
gdc.identifier.openalex W4406230575
gdc.index.type WoS
gdc.oaire.accesstype GOLD
gdc.oaire.diamondjournal false
gdc.oaire.impulse 2.0
gdc.oaire.influence 2.6892826E-9
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gdc.oaire.keywords aerodynamic performance
gdc.oaire.keywords multiple reference frame (MRF)
gdc.oaire.keywords TJ1-1570
gdc.oaire.keywords Mechanical engineering and machinery
gdc.oaire.keywords small axial-flow fan
gdc.oaire.keywords computational fluid dynamics (CFD)
gdc.oaire.keywords energy efficiency
gdc.oaire.keywords flow control
gdc.oaire.popularity 4.156965E-9
gdc.oaire.publicfunded false
gdc.openalex.collaboration National
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gdc.openalex.normalizedpercentile 0.78
gdc.opencitations.count 0
gdc.plumx.mendeley 8
gdc.plumx.newscount 1
gdc.plumx.scopuscites 2
publicationissue.issueNumber 1
publicationvolume.volumeNumber 10
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relation.isOrgUnitOfPublication.latestForDiscovery ac5ddece-c76d-476d-ab30-e4d3029dee37

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