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).


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    Title :

    Application of Uncertainty Quantification Methodologies to Falcon


    Contributors:
    Rogé, G. (author) / Loyatho, X. (author)


    Publication date :

    2018-07-21


    Size :

    15 pages





    Type of media :

    Article/Chapter (Book)


    Type of material :

    Electronic Resource


    Language :

    English




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