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foam-extend4.1-coherent-io/validationAndVerificationSuite/validation/overset/NACA4412-airfoil/NOTES

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Reference experimental data:
https://turbmodels.larc.nasa.gov/naca4412sep_val.html
Overset:
- Low Reynolds mesh with y+ << 1
Single mesh:
- High Reynolds with y+ approximately 16
Work in progress: comparing velocity profiles at certain chord lengths.