Flutter Analysis of Flexible Wing Configurations Using Pre-Stressed Structures Technique
The goal of this work is to define an improved methodology of flutter effect computing by taking into consideration the pre-stressed effect at a high deformed structure.
Authors
- Mircea BOCIOAGA
- Tudor Vladimirescu (ORCID: https://orcid.org/0009-0008-5596-4540)
- Radu Adrian Bocioaga
Institutions
- National Institute for Aerospace Research Elie Carafoli (RO)
Publication Details
- Journal
- Zenodo (CERN European Organization for Nuclear Research)
- Published
- 2026-11-04
- DOI
- https://doi.org/10.5281/zenodo.23945654
- Primary Topic
- Aeroelasticity and Vibration Control
- Type
- article
- Field-Weighted Citation Impact
- 0.00