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openfoamtutorials/airfoil_validation

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airfoil_validation

NACA0012 OpenFOAM results are compared to experimental data.

  1. Set the desired angle of attack: variable "aoa" (degrees) in mesh/parameters.geo.
  2. ./run.sh (see script for sub-steps)
  3. Open "view.foam" in ParaView and/or view force coefficients in ./case/postProcessing/.

TODO:

  1. Implement batch run, post-processing, and plotting script.

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NACA0012 OpenFOAM results are compared to experimental data.

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