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fluent model selection
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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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