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A study was performed on the structural behavior of a wing profile NACA 4412 fabricated with aluminum 6061, to obtain stress measurements of an airfoil, which are processed by a data acquisition system PXI. A comparative analysis between theoretical estimates, analysis by the finite elements method using the software ANSYS and values measured with the data acquisition system PXI, for validating the methodology used in the measurement. Through a set of uniaxial gauges, a triaxial configuration was achieved, integrating this arrangement to the data acquisition system in order to monitor the information measured. According to the theoretical results, those of the ANSYS analysis and the experimental values, an acceptable degree of accuracy was achieved. These results validate the data acquisition through a setting gauge in the form of delta rosette for the stress analysis of an airfoil.

Análisis Comparativo Estructural Mediante Galgas Uniaxiales y Triaxiales para un Perfil de Ala NACA 4412