Non-Linear Analysis in Post-Buckling Regime of a Tilt Rotor Composite Wing Structure Using Detailed Model and Robust Loading Approach

Non-Linear Analysis in Post-Buckling Regime of a Tilt Rotor Composite Wing Structure Using Detailed Model and Robust Loading Approach

The design and development of a wing for a completely brand-new aircraft represents, in aeronautics, one of the highest challenges from an engineering point of view. The present work describes a novel methodology devoted to execute numeric simulation in a non-linear post-buckling regime to verify th...

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Bibliographic Details
Main Authors: Antonio Chiariello, Pasquale Vitale, Marika Belardo, Francesco Di Caprio, Mauro Linari, Claudio Pezzella, Jacopo Beretta, Luigi Di Palma
Format: Article
Language:English
Published: MDPI AG 2023-12-01
Series:Journal of Composites Science
Subjects:
post-buckling
composite
tilt-rotor
wing
inertia relief
DFEM
Online Access:https://www.mdpi.com/2504-477X/8/1/4

Internet

https://www.mdpi.com/2504-477X/8/1/4

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