A rapid aerodynamic prediction method for unconventional transonic aircraft configurations
Date
2018-12-31
Supervisor/s
Journal Title
Journal ISSN
Volume Title
Publisher
ICAS
Department
Type
Conference paper
ISSN
Format
Free to read from
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
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.
Description
© The Authors.
Software Description
Software Language
Github
Keywords
Transonic Aerodynamics, Aircraft Design, CFD
DOI
Rights
© The Authors.
Attribution 4.0 International
Attribution 4.0 International