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.
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.
Analyzing aerodynamics of Boeing 747 using first principles of fluid mechanics
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