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.
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