Vortex lattice CFD application and modeling validation for ground effect aircraft

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dc.contributor.authorZammit, Karl
dc.contributor.authorSmith, Howard
dc.contributor.authorLobo, Noel Sierra
dc.contributor.authorGiannopoulos, Ioannis K.
dc.date.accessioned2024-02-22T10:56:44Z
dc.date.available2024-02-22T10:56:44Z
dc.date.issued2024-02-09
dc.description.abstractThis paper explores the application of vortex lattice computational fluid dynamics method capability to model aircraft flight near to ground, utilizing the ground effect. Computational results were correlated with existing analytic formulations and benchmarked against experimental data from the public domain. A case aerodynamics design study was formed, based on the Russian A-90 Orlyonok Ekranoplan wing. The study provided a verification and a validation step towards advancing ground effect aircraft turnaround conceptual and preliminary design time, using the rapid aerodynamics results generation vortex lattice CFD method.en_UK
dc.identifier.citationZammit K, Smith H, Lobo NS et al., (2024) Vortex lattice CFD application and modeling validation for ground effect aircraft. WSEAS Transactions on Fluid Mechanics, Volume 19, February 2024, Article number 5, pp. 49-58en_UK
dc.identifier.issn1790-5087
dc.identifier.urihttps://doi.org/10.37394/232013.2024.19.5
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/20872
dc.language.isoenen_UK
dc.publisherWSEAS (World Scientific and Engineering Academy and Society)en_UK
dc.rightsAttribution 4.0 International*
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/*
dc.subjectEkranoplanen_UK
dc.subjectCFDen_UK
dc.subjectVortex Lattice methoden_UK
dc.subjectAVLen_UK
dc.subjectFlight Ground Effecten_UK
dc.subjectA-90 Orlyonoken_UK
dc.titleVortex lattice CFD application and modeling validation for ground effect aircraften_UK
dc.typeArticleen_UK
dcterms.dateAccepted2023-12-16

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