Abstract
The A-airfoil has served as a validation test case in previous EU projects, EUROVAL, ECARP and LESFOIL, using RANS approaches for the first two projects and LES methods in LESFOIL. Nevertheless, and demonstrated below, there is still considerable interest in further investigation of that airfoil case for both turbulence model validation and testing of numerical schemes and methods. In that respect, new RANS computations for the full three-dimensional geometry (wing in wind tunnel) resulted in obvious 3D effects t hat put the two-dimensional approaches “somewhat” in question, or vice versa.
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© 2006 Springer-Verlag Berlin Heidelberg
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Haase, W. (2006). The Aerospatiale A-airfoil. In: Haase, W., Aupoix, B., Bunge, U., Schwamborn, D. (eds) FLOMANIA — A European Initiative on Flow Physics Modelling. Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM), vol 94. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-540-39507-2_42
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DOI: https://doi.org/10.1007/978-3-540-39507-2_42
Publisher Name: Springer, Berlin, Heidelberg
Print ISBN: 978-3-540-28786-5
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