Project Details
Description
The creep forming process of an aeronautic component was investigated and optimized using a numerical tool based on Finite Elements that was developed in a previous project. The results from the optimization showed that a siginificant process time reduction was possible.
| Status | Finished |
|---|---|
| Effective start/end date | 27/07/20 → 23/07/21 |
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Projects
- 1 Finished
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AFRC-DIRF-1428 Creep Forming Thermo-Mechanical Analysis
Sancho, A. (Principal Investigator) & Gonzalez, D. (Co-investigator)
15/07/19 → 29/05/20
Project: Research