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June 20, 2021, 07:40
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Mesh validation
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New Member
Join Date: Jun 2021
Posts: 8
Rep Power: 4  |
Hi,
I am new to CFD simulations and I would like to as some questions. For an university project I have to validate a mesh against experimental results (lift coefficient and drag coefficient) of a NACA63-415 airfoil. The experimental results I have found were obtained with an airfoil having a chord length of 0.606m, Re=1.6e6 and inlet velocity 40 m/s. For the cfd simulations, can I use an airfoil with a 1m chord? I would use the same Reynolds number changing the inlet velocity. Thanks in advice. |
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| Tags |
| airfoil geometry, mesh validation, starccm+ |
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