✈️ 2D Aero Analysis & Optimizer Suite

2D Airfoil Simulation and UAV OPTIMIZER — Set parameters and click 'Predict'
Validate results with CFD/Wind Tunnel tests for critical applications.

🔺 Lift Coefficient (CL)

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🔻 Drag Coefficient (CD)

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Parameter Sweep for NACA 0012

🚁 UAV Design Optimization

📊 Model & Application Information

Input Features:

  • Airfoil: cross‑sectional shape (index 0‑9).
  • Thickness ratio (t/c): automatically set from airfoil last two digits.
  • Mach Number: flight speed relative to sound.
  • Reynolds Number: absolute value.
  • Angle of Attack (α): angle between airfoil and airflow.

⚠️ Placeholder formulas for demonstration. Validate with CFD/wind tunnel for critical applications.