Wednesday, September 17, 2025

CFD Analysis of NACA 4412 Airfoil using Ansys Fluent

 


  • Domain: Aerodynamics / CFD
  • Software Required: Ansys Fluent / XFLR5
  • Objective: Analyze lift & drag characteristics at various angles of attack.
  • Expected Outcome: Pressure distribution, aerodynamic efficiency graphs.
  • Applications: Aircraft wing optimization, UAV design.
    👉 For complete report, PPT & files → Contact Us


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