Parallel Mesh Adaptive Techniques Illustrated with Complex Compressible Flow Simulations

Table 1

Final grid sizes for different number of processors after 4 adaptation steps. 2D NACA 0012 airfoil.

Processors	N_nodes	N_elements	N_surf_el
1	35 130	69 615	645
2	35 082	69 527	637
4	34 335	68 031	639
8	34 839	69 035	643