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.
Higher-Order Stabilized Finite Elements in an Industrial Navier-Stokes Code
ADIGMA - A European Initiative on the Development of Adaptive Higher-Order Variational Methods for Aerospace Applications ; 2 ; 145-165
2010-01-01
21 pages
Article/Chapter (Book)
Electronic Resource
English
Goal-Oriented Mesh Adaptation in an Industrial Stabilized Finite Element Navier-Stokes Code
Springer Verlag | 2010
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