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Panel method for steady multi-component 2D airfoil analysis using a linear vortex distribution | Python version

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theo_a_python

A simple tool for analysis of 2D airfoils using potential flow theory

Methodology: Linear vorticity distribution

Version: Python prepro, solver & postpro

References: "Low Speed Aerodynamics - From wing theory to panel methods", Joseph Katz, et. al., 1991, McGraw-Hill

Validation case: NACA 0012, Re = 500E3

  • N_points = 50
  • elapsed_time ~ 125 [s]

Results:

cpvsx

clvsalpha

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Panel method for steady multi-component 2D airfoil analysis using a linear vortex distribution | Python version

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