Context
Large and thick aeronautical parts present distortion after machining because the residual stresses (RS) generated during previous manufacturing steps (heat treatment).
Before assembly, distortion is removed manually.
It is a time consuming operation and depends exclusively on the skills of a well trained operator.
Scientific goals
To develop a Reduced Order Model (ROM) for reshaping
To evaluate the main parameters during the process and its uncertainty level
Industrial goals
To study reshaping from a numerical perspective
To adapt reshaping simulations to each warped geometry
To introduce numerical simulation in order to assist the operato
