Laboratorio virtual para la interpretación de las cargas en vuelo

The subject \Flight Loads" framed in the Master in Aerospace Engineering is based largely on the concepts seen in courses like Flight Mechanics or Structural Analysis of the Degree in Aerospace Engineering. On the one hand, the equations involved can not be solved by traditional methods but on the other hand we need our students to acquire specic competences derived from the interpretation of these equations. In the present article we propose a simple numerical and graphic tool developed in the Mathematica software environment that allows interactively solving the Flight Mechanics equations of an airplane and obtain results directly related to the structural design. Several examples show how the presented model works.