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Pressure Coefficient $ C_p$ around the Airfoil Profile

  • Pressure coefficient $ C_p$ around the airfoil profile is evaluated.
  • The NASA experiment results are available as well as NASA RANS simulation results are available.
NACA4412 Pressure coefficient Cp NASA experiment data

Figure: Pressure coefficient $ C_p$ versus dimensionless x-axis. The x-axis was divided by the length of the chord of the NACA4412 profile. Dataset NASA exp is the experimental data. Dataset NASA SA is the NASA RANS simulation results with Spalart Allmaras turbulence model.