Experimental and numerical investigation of an aircraft wing with hinged wingtip for gust load alleviation-Reference-Cited by-同舟云学术

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Experimental and numerical investigation of an aircraft wing with hinged wingtip for gust load alleviation

Published:2023-05 Issue: Volume:119 Page:103892
ISSN:0889-9746
Container-title:Journal of Fluids and Structures
language:en
Short-container-title:Journal of Fluids and Structures

Author:

Balatti Davide^ORCID,Khodaparast Hamed Haddad,Friswell Michael I.,Manolesos Marinos^ORCID,Castrichini Andrea

Publisher

Elsevier BV

Subject

Mechanical Engineering

Reference29 articles.

1. Flight dynamics of transport aircraft equipped with flared-hinge folding wingtips;Ajaj;J. Aircr.,2021

2. Articulating winglets;Allen,1999

3. Knee-action wings cushion ride in french plane;Anon;Pop. Sci. Mag.,1951

4. Active hinged wingtip for gust load alleviation and manoeuvres;Balatti,2023

5. Improving wind tunnel “1-cos” gust profiles;Balatti;J. Aircr.,2022

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1. Experimental and numerical gust identification using deep learning models;Applied Mathematical Modelling;2024-08

2. Aerodynamic Optimization and Characterization of a Ducted Tail for a Box-Launched Aircraft;Applied Sciences;2024-07-25

3. A Time-Domain Calculation Method for Gust Aerodynamics in Flight Simulation;Aerospace;2024-07-16

4. Nonlinear Aeroelastic Response Analysis of Wing with Flared Folding Wingtip;Journal of Aerospace Engineering;2024-05

5. Aeroelastic Scaling of a High-Aspect-Ratio Wing Incorporating a Semi-Aeroelastic Hinge;AIAA Journal;2024-04-17

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