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Fig. 8 | Advances in Aerodynamics

Fig. 8

From: An ultralight geometry processing library for parallel mesh refinement

Fig. 8

An example illustrating the parallel mesh refinement workflow. a is the input coarse mesh. b is the partitioned result of the input mesh. c is the refinement result of (b). d is the final mesh after projecting new surface points onto the original CAD model. Note that a mesh deformation is carried on after projection to improve shape quality of volume elements

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