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Aerodynamics Wind Tunnel

NACA airfoil & flow visualization·Zeq OS·v1.287.5

ActiveEngineering

About

Virtual wind tunnel with NACA 4-digit airfoil generation, thin airfoil theory lift prediction, pressure coefficient distribution, and Blasius boundary layer thickness computation. Canvas flow field visualization with streamlines around the airfoil and pressure coloring.

Key Features

  • NACA 4-digit airfoil generator
  • Thin airfoil theory lift prediction
  • Pressure coefficient (Cp) distribution
  • Blasius boundary layer computation
  • Canvas streamline flow visualization

Algorithms

NACA 4-digit airfoil generatorPanel method flow solverStreamline integrationCp pressure distribution

Key Operators

AERO-NACAAERO-BLASIUSAERO-CL

Technical Details

Zeq OS
Framework
1,576
Operators
64
Categories
1.287 Hz
Sync Rate
≤0.1%
Precision

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