vortex-panel-method

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Eliasfarah0 / Vortex-Panel-Method-for-Airfoil-Aerodynamic-Coefficients

This repository makes use of the Vortex Panel Method to calculate the Lift, Drag and Pressure Coefficients of any airfoil at a specified Freestream Velocity, Chord Length and Angle of Attack by providing the X and Y coordinates of the airfoil in a .dat file.

matlab airfoil vortex-panel-method

Updated Jul 22, 2021
MATLAB

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vortex-panel-method

Here is 1 public repository matching this topic...

Eliasfarah0 / Vortex-Panel-Method-for-Airfoil-Aerodynamic-Coefficients

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