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.accessioned2025-03-17T12:25:33Z
dc.date.available2025-03-17T12:25:33Z
dc.date.issued2023
dc.departmentTarsus Üniversitesi
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%.
dc.identifier.doi10.1177/09544089231190182
dc.identifier.issn0954-4089
dc.identifier.issn2041-3009
dc.identifier.scopus2-s2.0-85166623862
dc.identifier.scopusqualityQ2
dc.identifier.urihttps://doi.org/10.1177/09544089231190182
dc.identifier.urihttps://hdl.handle.net/20.500.13099/1733
dc.identifier.wosWOS:001040609600001
dc.identifier.wosqualityQ2
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakScopus
dc.language.isoen
dc.publisherSage Publications Ltd
dc.relation.ispartofProceedings of The Institution of Mechanical Engineers Part E-Journal of Process Mechanical Engineering
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.snmzKA_WOS_20250316
dc.subjectAnti-icing
dc.subjectNACA0015
dc.subjectimpinging jet
dc.subjectconvective heat transfer
dc.subjectCFD
dc.titleThermohydraulic performance assessment of new alternative methods for anti-icing application against current application in an aircraft
dc.typeArticle

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