Following the implementation of Katz and Plotkin, this code simulates the performance of an aerofoil in steady flow assuming that the flow remains attached and viscous effects can be ignored.
Alexander Giles (2021). Panel method for NACA XXXX aerofoils (https://www.mathworks.com/matlabcentral/fileexchange/52771-panel-method-for-naca-xxxx-aerofoils), MATLAB Central File Exchange. Retrieved .
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