A rapid aerodynamic prediction method for unconventional transonic aircraft configurations

Prince, Simon A.; Di Pasquale, Davide; Garry, Kevin; Nuzzo, Cristina

CERES Home
→
School of Aerospace, Transport and Manufacturing (SATM)
→
Staff publications (SATM)
→
View Item

dc.contributor.author	Prince, Simon A.
dc.contributor.author	Di Pasquale, Davide
dc.contributor.author	Garry, Kevin
dc.contributor.author	Nuzzo, Cristina
dc.date.accessioned	2019-03-13T15:35:45Z
dc.date.available	2019-03-13T15:35:45Z
dc.date.issued	2018-12-31
dc.identifier.citation	Prince 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, Brazil	en_UK
dc.identifier.uri	https://dspace.lib.cranfield.ac.uk/handle/1826/13986
dc.identifier.uri	https://www.icas.org/ICAS_ARCHIVE/ICAS2018/data/preview/ICAS2018_0138.htm
dc.description	© The Authors.
dc.description.abstract	This 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.language.iso	en	en_UK
dc.publisher	ICAS	en_UK
dc.rights	© The Authors.
dc.rights	Attribution 4.0 International
dc.rights.uri	http://creativecommons.org/licenses/by/4.0/
dc.subject	Transonic Aerodynamics	en_UK
dc.subject	Aircraft Design	en_UK
dc.subject	CFD	en_UK
dc.title	A rapid aerodynamic prediction method for unconventional transonic aircraft configurations	en_UK
dc.type	Conference paper	en_UK