Discrete vortex method codes for calculating lift coefficient of thin lifting airfoils
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Updated
Dec 19, 2022 - MATLAB
Discrete vortex method codes for calculating lift coefficient of thin lifting airfoils
Analysis And Computation Of Aerodynamics Parameters of a 4-digit NACA Airfoil With Flaps Using The Discrete Vortex Method (DVM)
This repository contains the code used for simulations in the study by Aksnes et al. (2023)
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