Prince, Simon A.Di Pasquale, DavideGarry, KevinNuzzo, Cristina2019-03-132019-03-132018-12-31Prince 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, Brazilhttps://dspace.lib.cranfield.ac.uk/handle/1826/13986https://www.icas.org/ICAS_ARCHIVE/ICAS2018/data/preview/ICAS2018_0138.htmThis 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© The Authors.Attribution 4.0 Internationalhttp://creativecommons.org/licenses/by/4.0/Transonic AerodynamicsAircraft DesignCFDConference paper