Implement the Thin Airfoil Theory given the coordinates of the profile to be analysed.
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Updated
Dec 3, 2020 - Python
Implement the Thin Airfoil Theory given the coordinates of the profile to be analysed.
A set of tools that let you analyze the aerodynamic performance of wings and airfoils using models such as TaT,LLT and VLM.
ME529 Aerodynamics in C - Coursework 1 - Thin Aerofoil Theory
This paper is prepared as part of CA course and it contains a study on the classical thin airfoil theory for a cambered airfoil, NACA 1408.
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