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.
Alvaro Moral Aranda, Agustín Pérez Arjona, Vincenzo Rosciano, Alvaro Sanjuán Florido and Alfonso Velencoso Gómez.
A good way to improve LaTeX skills is to write classroom assignments and reports in LaTeX. This template can help you get started.
Feel free to suggest improvements at vishal dot sharma at aggiemail.usu.edu
This repository contains LaTeX template for NIT Trichy's M.S. (By Research)/PhD Thesis. This template has been created considering latest guidelines. The first prepared thesis using this template was submitted and accepted by MS/PhD section in May 2019. This template can also be used by B.Tech./M.Tech. students for their thesis preparation.