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FastS: CRM Wing-Body Fuselage

RANS simulation around the CRM DPW5 configuration at Mach=0.85, Reynolds=5.e6 and 2.154° of angle of attack.

Geometry & Mesh


Original Image Solution
Modified Image Mesh

             
Geometry + Multiblock structured Mesh (41M points)

         

Results




              Density Isocontours at wall.


              Cp at 25% span. Comparison with reference elsA solver.

              Cp at 50% span. Comparison with reference elsA solver.

              Cp at 75% span. Comparison with reference elsA solver.

              Cp at 95% span. Comparison with reference elsA solver.
                                                                                                                                                                                                                 

Computation

CPU time (12 cores) for 16000 iterations : 105 min.

         
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