A rapid aerodynamic prediction method for unconventional transonic aircraft configurations

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dc.contributor.authorPrince, Simon A.
dc.contributor.authorDi Pasquale, Davide
dc.contributor.authorGarry, Kevin
dc.contributor.authorNuzzo, Cristina
dc.date.accessioned2019-03-13T15:35:45Z
dc.date.available2019-03-13T15:35:45Z
dc.date.issued2018-12-31
dc.description.abstractThis paper presents some results comparing the use of the Full Potential equations, coupled with the turbulent integral boundary layer equations for aircraft transonic cruise analysis. Use of such a method in the conceptual design stage is shown to be capable of yielding accurate enough data in a few minutes on a single processor, where Navier - Stokes simulations on 100+ processors take several days.en_UK
dc.identifier.citationPrince S, Di Pasquale D, Garry K, Nuzzo C. (2018) A rapid aerodynamic prediction method for unconventional transonic aircraft configurations. 31st Congress of the International Council of the Aeronautical Sciences, 9-14 September 2018, Belo Horizonte, Brazilen_UK
dc.identifier.urihttps://dspace.lib.cranfield.ac.uk/handle/1826/13986
dc.identifier.urihttps://www.icas.org/ICAS_ARCHIVE/ICAS2018/data/preview/ICAS2018_0138.htm
dc.language.isoenen_UK
dc.publisherICASen_UK
dc.rights© The Authors.
dc.rightsAttribution 4.0 International
dc.rights.urihttp://creativecommons.org/licenses/by/4.0/
dc.subjectTransonic Aerodynamicsen_UK
dc.subjectAircraft Designen_UK
dc.subjectCFDen_UK
dc.titleA rapid aerodynamic prediction method for unconventional transonic aircraft configurationsen_UK
dc.typeConference paperen_UK

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