Abstract
This chapter covers Dassault Aviation’s contribution to Workpackage 3 of the ADIGMA Project, which focuses on the extension of its stabilized finite element industrial Navier-Stokes code to higher-order elements. Mesh generation aspects are treated and especially the issue of highly-stretched curved elements close to the wall boundary of Navier-Stokes meshes. The high-order approach is carefully assessed using inviscid subsonic and transonic, laminar, and high Reynolds number turbulent flows.
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Chalot, F., Normand, PE. (2010). Higher-Order Stabilized Finite Elements in an Industrial Navier-Stokes Code. In: Kroll, N., Bieler, H., Deconinck, H., Couaillier, V., van der Ven, H., Sørensen, K. (eds) ADIGMA - A European Initiative on the Development of Adaptive Higher-Order Variational Methods for Aerospace Applications. Notes on Numerical Fluid Mechanics and Multidisciplinary Design, vol 113. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-03707-8_11
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DOI: https://doi.org/10.1007/978-3-642-03707-8_11
Publisher Name: Springer, Berlin, Heidelberg
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