vahadruya / Airfoil_results_XFOIL

Visualisation of general XFOIL results

lift-coefficient numerical-integration plotly polar-plots trapezoidal-rule xfoil pressure-coefficient

Airfoil results XFOIL

Rough visualisation of general results from XFOIL.

Polar plots, calculation of modCL from Cp, reasoning and result understanding of flaps and slats on airfoils

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Visualisation of general XFOIL results

lift-coefficient numerical-integration plotly polar-plots trapezoidal-rule xfoil pressure-coefficient

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