In the heart of the Technical Direction and more specifically in the Combustion and Nozzle Design Office, you will be integrated in the Combustor Development Team.
The Combustion Design Office is in charge of designing, specifying and integrating combustors for military and civil applications.

One of the key requirements for a combustor is to ensure mechanical durability.
In the design phase, predicting combustor durability is challenging. Particularly because complexe elasto-visco-plastic (EVP) computations are needed.
In this context, the combustion design office is developping a new methodology for improved and simpler EVP computations.

Under the supervision of a mechanical engineer, you will contribute to testing, implementing and improving this methodology.

You have or are preparing a masters degree in aeronautical engineering, with a specialization in mechanics.
You like technical challenges and are familiar with finite element method.