This code is used to solve the boundary layer over an airfoil section in the three regimes subsonic regime, transition regime and turbulent regime
Mohamed Atyya (2021). Solution of the boundary layer over an airfoil section (https://www.mathworks.com/matlabcentral/fileexchange/58130-solution-of-the-boundary-layer-over-an-airfoil-section), MATLAB Central File Exchange. Retrieved .
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