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- W2217356 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." @default.
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- W2217356 date "2010-01-01" @default.
- W2217356 modified "2023-10-18" @default.
- W2217356 title "Higher-Order Stabilized Finite Elements in an Industrial Navier-Stokes Code" @default.
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- W2217356 doi "https://doi.org/10.1007/978-3-642-03707-8_11" @default.
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