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© The Authors.
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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