Approximating the Circulation along the span wise axis for a Finite Length Wing using Prandtl Lifting-Line theory.
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Updated
Jul 17, 2020 - Python
Approximating the Circulation along the span wise axis for a Finite Length Wing using Prandtl Lifting-Line theory.
Finite-wing aerodynamic analysis with spanwise variations and aileron deflections using Fourier decomposition
Implementación en MATLAB de los métodos de Multhopp y Vortex Lattice para el análisis aerodinámico de alas de envergadura finita.
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