Mesh adaptation to a solution

We want to adapt a M6 wing mesh (named aileM6.mesh) to an isotropic size map given in the aileM6-met.sol file (see figure 1 for the mesh and the metric representation).

Figure 1: Initial mesh of the M6 wing and associated metric : surface of the wing (left) and cut through the volume mesh (right)

Figure 1: Initial mesh of the M6 wing and associated metric : surface of the wing (left) and cut through the volume mesh (right)

Note that our metric is obtained from the density solution using the mshmet software (thanks to C. Dapogny, C.Dobrzynski and P. Frey).
You can adapt the mesh with the following command:

mmg3d_O3 aileM6.mesh -sol aileM6-met.sol -hgrad 2.3 -v 3

The final mesh is displayed figure 2.

Figure 2: Final mesh of the M6 wing: surface of the wing (left) and cut through the volume mesh (right)

Figure 2: Final mesh of the M6 wing: surface of the wing (left) and cut through the volume mesh (right)

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