Abstract
In this section, we give both the description of the IC-03 Falcon test case (Industrial Challenge [1]) and comparison of results (Delft UMRIDA workshop, [2] and other partner’s inputs). A database incorporating modelization (turbulence), numerical error (mesh), operational (AoA), and geometrical (wing spanwise twist distribution) uncertainties have been created. Six Partners are involved in IC-03: Alenia Aermacchi/Leonardo (Italy), INRIA (France), NUMECA (Belgium), TU Delft (Netherlands), VUB (Belgium), Dassault Aviation (France).
Cite
CITATION STYLE
Rogé, G., & Loyatho, X. (2019). Application of uncertainty quantification methodologies to Falcon. In Notes on Numerical Fluid Mechanics and Multidisciplinary Design (Vol. 140, pp. 383–397). Springer Verlag. https://doi.org/10.1007/978-3-319-77767-2_24
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