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Application of Uncertainty Quantification Methodologies to Falcon

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Part of the book series: Notes on Numerical Fluid Mechanics and Multidisciplinary Design ((NNFM,volume 140))

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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References

  1. Umrida Project: Test Case Description Innovative Database For UQ and RDM: IC-03

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  2. UMRIDA Delft Workshop on UQ: IC-03 Falcon Test Case Presentation

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Correspondence to G. Rogé .

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Rogé, G., Loyatho, X. (2019). Application of Uncertainty Quantification Methodologies to Falcon. In: Hirsch, C., Wunsch, D., Szumbarski, J., Łaniewski-Wołłk, Ł., Pons-Prats, J. (eds) Uncertainty Management for Robust Industrial Design in Aeronautics . Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 140. Springer, Cham. https://doi.org/10.1007/978-3-319-77767-2_24

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  • DOI: https://doi.org/10.1007/978-3-319-77767-2_24

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  • Publisher Name: Springer, Cham

  • Print ISBN: 978-3-319-77766-5

  • Online ISBN: 978-3-319-77767-2

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