2D Airfoil Transition Cases
=================================

.. comment include:: ../../nalu-wind/2D_airfoil_Transition/README.md
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#. `NLF(1)-0416 airfoil <2D_airfoil_Transition/NLF1-0416/README.html>`__: Validation and verification of the 1-equation gamma transition model on the NASA NLF(1)-0416 airfoil.

   * `Simulation conditions <2D_airfoil_Transition/NLF1-0416/README.html#simulation-conditions>`__
   * `Running the simulation <2D_airfoil_Transition/NLF1-0416/README.html#running-the-simulation>`__
   * `Results <2D_airfoil_Transition/NLF1-0416/README.html#results-grid-sensitivity-study>`__

#. `TU Delft DU00-W-212 airfoil <2D_airfoil_Transition/DU00-W-212/README.html>`__: Validation of the 1-equation gamma transition model on the TU Delft DU00-W-212 airfoil with a full angle-of-attack sweep.
   
   * `Simulation conditions <2D_airfoil_Transition/NLF1-0416/README.html#results-grid-sensitivity-study>`__
   * `Running the simulation <2D_airfoil_Transition/DU00-W-212/README.html#simulation-conditions>`__
   * `Results <2D_airfoil_Transition/DU00-W-212/README.html#results-angle-of-attack-sweep>`__
   
   
`View these cases in the github repository
<https://github.com/Exawind/exawind-benchmarks/tree/main/nalu-wind/2D_airfoil_Transition>`__

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