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49–58 of 58 projects for “dissertation” · sorted by most relevant

M.Tech / M.E.

Aerospace / Aeronautical

NACA 0012 Airfoil CFD Validation Study Against XFOIL with Mesh Convergence

A mesh-converged OpenFOAM study of the NACA 0012 aerofoil validated against XFOIL and NASA's turbulence-modelling reference data

  • OpenFOAM v12 (finite-volume CFD, SA and k-ω SST models)
  • XFOIL 6.99 (panel method with integral boundary layer)
  • Gmsh and blockMesh for structured C-grid generation
  • +3

advanced24 wkSolo