Thermohydraulic performance assessment of new alternative methods for anti-icing application against current application in an aircraft

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dc.authoridARSLAN, Kamil/0000-0002-1216-6812
dc.contributor.authorPazarlioglu, Hayati Kadir
dc.contributor.authorTepe, Ahmet Umit
dc.contributor.authorArslan, Kamil
dc.date.accessioned2024-09-29T16:05:02Z
dc.date.available2024-09-29T16:05:02Z
dc.date.issued2023
dc.departmentKarabük Üniversitesien_US
dc.description.abstractIn this study, anti-icing problems, which are mostly industrial problems in aerospace companies, have been numerically investigated. Herein, to enhance anti-icing performance of NACA0015, different jet-to-surface distances (H/d), jet angles (& alpha;), and slot jet designs with different aspect ratios (ARs) have also been investigated. ANSYS Fluent 2020R2 commercial program has been utilized for all numerical calculations. In addition, the SST k-& omega; with low-Re correction wall treatment turbulence model has been used for solving turbulence equation. Furthermore, the average Nusselt number (Nu) on the NACA0015's surface, pressure drop, and performance evaluation criteria (PEC) which define the anti-icing performance of novel proposed system have been presented section by section. As a result of the investigation, it has been obtained that the use of AR = 4 increases the Nu by 85.52% compared to circular jet for the H/d = 4 at & alpha; = 90 & DEG;. The pressure drop value dramatically increases using AR = 4 around 307.85% compared to circular jet for H/d = 4 at & alpha; = 90 & DEG;. Despite this drastic increment in pressure drop, the PEC value is kept as 1.14 using AR = 4, H/d = 4, and & alpha; = 90 & DEG;. Finally, empirical correlations developed from existing findings have been presented with an error rate of lower than 5%.en_US
dc.identifier.doi10.1177/09544089231190182
dc.identifier.issn0954-4089
dc.identifier.issn2041-3009
dc.identifier.scopus2-s2.0-85166623862en_US
dc.identifier.scopusqualityQ3en_US
dc.identifier.urihttps://doi.org/10.1177/09544089231190182
dc.identifier.urihttps://hdl.handle.net/20.500.14619/6468
dc.identifier.wosWOS:001040609600001en_US
dc.identifier.wosqualityQ2en_US
dc.indekslendigikaynakWeb of Scienceen_US
dc.indekslendigikaynakScopusen_US
dc.language.isoenen_US
dc.publisherSage Publications Ltden_US
dc.relation.ispartofProceedings of the Institution of Mechanical Engineers Part E-Journal of Process Mechanical Engineeringen_US
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanıen_US
dc.rightsinfo:eu-repo/semantics/closedAccessen_US
dc.subjectAnti-icingen_US
dc.subjectNACA0015en_US
dc.subjectimpinging jeten_US
dc.subjectconvective heat transferen_US
dc.subjectCFDen_US
dc.titleThermohydraulic performance assessment of new alternative methods for anti-icing application against current application in an aircraften_US
dc.typeArticleen_US

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