Aeroelastic and Dynamic Structural Analysis of a non-tapered wing
Author
Alvaro Moral Aranda, Agustín Pérez Arjona, Vincenzo Rosciano, Alvaro Sanjuán Florido and Alfonso Velencoso Gómez.
Last Updated
5年前
License
Creative Commons CC BY 4.0
Abstract
In this document a thorough analysis of flutter will be presented, applied on a wing box which has been discretized using a FEM tool, MSC. NASTRAN, to cover both the dynamic structural analysis as well as the aeroelastic solution to flutter. Once the structural part has been detailed, a discussion about the flutter speed obtained with the Nastran SOL 145 will be presented, followed by some other solutions.