A Parametric Study on the Aeroelasticity of Flared Hinge Folding Wingtips

A Parametric Study on the Aeroelasticity of Flared Hinge Folding Wingtips

This paper presents a parametric study on the aeroelasticity of cantilever wings equipped with Flared Hinge Folding Wingtips (FHFWTs). The finite element method is utilized to develop a computational, low-fidelity aeroelastic model. The wing structure is modelled using Euler–Bernoulli beam elements,...

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Bibliographic Details
Main Authors: Rafic M. Ajaj, Erick I. Saavedra Flores, Mohammadreza Amoozgar, Jonathan E. Cooper
Format: Article
Language:English
Published: MDPI AG 2021-08-01
Series:Aerospace
Subjects:
folding wingtips
flared hinge
finite element method
aeroelasticity
structural nonlinearities
Online Access:https://www.mdpi.com/2226-4310/8/8/221

Internet

https://www.mdpi.com/2226-4310/8/8/221

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