This paper presents an experimental method to measure deformations of the wing in different speeds inside the wind tunnel. Thronging it, we can define the aeroelastic properties of the wing to check these theoretical methods in studying the aeroelastic problems; furthermore, we also check these specific problems in the elastic and the distributive of the aerodynamic load while wing is deformed. Key words: Aeroelastic, Discrete vortex method, Elastic deformation, Experimental model
