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14th International Meshing Roundtable
San Diego, CA, USA
September 11-14, 2005
Jochen Wild
DLR, Institute for Aerodynamics and Flow Technology, Lilienthalplatz 7,
D-38108 Braunschweig, Germany
Peter Niederdrenk, Thomas Gerhold
DLR, Institute for Aerodynamics and Flow Technology, Bunsenstr.10, D-
37073 Göttingen, Germany
Abstract
Elliptic differential equations are derived for the generation of structured
meshes and difference equations for the generation of smooth hybrid
meshes from metric identity. A parabolic procedure is used to march the
solution of the difference equations simultaneously for both types of
meshes away from surface patches meshed by quads or triangles. An aerodynamic
application for the ONERA M6 wing demonstrates how the
blocking at the wing tip is simplified by using both types of meshes instead
of a purely structured mesh. On the other hand it is shown that a
large number of points can be saved compared to a purely hybrid grid.
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