Project of designing, building and analysis of a metallic stringer for aerospace applications. Loading and verification until range of elastic instability.

Abstract

The research in light weight structures is a crucial characteristic of the aerospace industry. The stringers with web buckling capability appeared as a result of this constant research. In this project, it is analyzed analytically, experimentally and numerically this kind of optimized structures to finish with the designing and building of an improved design which will serve as the basis for a laboratory practice in the subject of aerospace structures