Study of the modelling of the behaviour of a jet engine

This thesis explores the necessities of simulators of the behaviour of turbomachinery and proposes an implementation of such a simulator. This simulator consists in the model of a turbojet, which is described and implemented, and an algebra subsystem that takes the model and produces a viable solution. Models for the different components of a turbojet are described. An algebra subsystem analogous to SPICE for electric circuits is proposed and developed. The results are examined, analyzed and discussed