Introduction to Comsol Turbulent Simulation Around A Naca 0012 Airfoil

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Re = 100k, AoA = 4 degrees, Tu = 0.1%

Summary & Highlights for Comsol Turbulent Simulation Around A Naca 0012 Airfoil

  • Mesh adaptation for NACA 0012 airfoil in supersonic flow
  • NACA 0012 Airfoil Simulation
  • RANS, URANS, and DES
  • NACA 0012 Airfoil Simulation
  • What really happens when an

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