|August 25, 2013, 03:28||
fluent model selection
Join Date: Jun 2013
Posts: 3Rep Power: 4
I am handling final year project of BLENDED WING BODY. Here I am using reference paper to validate results. In the reference paper they have used Euler-based parallel Newton-Krylov-Schur and other schemes that is shown in pic .Now I am confused at two points.
1.Do I use steady or transient flow solution?
2.Which model and solution methods I use ?
Please anyone help me with this
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