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April 15, 2020, 19:33
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Simulating post-stall results
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New Member
Jesus Roman
Join Date: Apr 2020
Posts: 2
Rep Power: 0  |
Hi all,
I am conducting a project about the aerodynamic effects on different elading edge geometries. I have two 3D models (wavy and sawtooth leading edge) which I am simualting in ANSYS Fluent. The results for the baseline wing does not match already existing results in post-stall regions. How can i obtain the correct results for this situation? Model: SST k-omega Re = 2e+05 y+ ~ 1 Boundary conditions in 3D C-grid: v-inlet, p-outlet, symmetry (in lateral faces), p-outlet (in top and bottom faces) Thank you. Jesus Roman |
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| fluent - parallel, post procesing, stall control |
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