FastS/IBM: ONERA M6 Wing

RANS flow around the ONERA M6 wing at Mach=0.8395, Reynolds=11.72M and 3.06° of angle of attack.

Mesh

Automatic Octree mesh + full Immersed Boundaries of 56M points (with a symmetry plane at wing root).
Snear = 0.001*c at leading and trailing edges and wing tip and trailing edge and 0.002*c elsewhere.
         

Cp results




              Isocontours Cp at wall.

              Cp at 20% span. Comparison between multiblock structured, full IBM computations and experiment.

              Cp at 44% span.

              Cp at 90% span.

              Cp at 65% span.

              Cp at 95% span.

              Cp at 80% span.

              Cp at 99% span.
         

Computation

Full IBM FastS: CPU time (56 cores) for 5000 iterations : 34min.

         
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