Experimental and virtual testing of a composite-aluminium aircraft wingbox under thermal loading-Reference-Cited by-同舟云学术

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Experimental and virtual testing of a composite-aluminium aircraft wingbox under thermal loading

Published:2023-07 Issue: Volume:138 Page:108329
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Guerrero José M.^ORCID,Sasikumar Aravind,Llobet Jordi^ORCID,Costa Josep^ORCID

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference44 articles.

1. Conceptual studies of a composite-aluminum hybrid wing box demonstrator;Kapidžić;Aerosp. Sci. Technol.,2014

2. Structural behaviour modelling of bolted joints in composite laminates subjected to cyclic loading;Scarselli;Aerosp. Sci. Technol.,2015

3. Experimental and numerical analysis of the mechanical behavior of composite-to-titanium bolted joints with liquid shim;Liu;Aerosp. Sci. Technol.,2016

4. Numerical model for investigation of the strain distribution in thick composite plates subjected to bolt loads;Gorjipoor;Aerosp. Sci. Technol.,2016

5. Numerical and experimental investigation of fitting tolerance effects on damage and failure of CFRP/Ti double-lap single-bolt joints;Cao;Aerosp. Sci. Technol.,2018

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1. Experimental and virtual testing of mode II and mixed mode crack propagation under dynamic loading;International Journal of Impact Engineering;2024-11

2. Investigation on bearing capacity and fracture behaviour of the bolt in a flange connection considering multiple load cases;Structures;2024-04

3. An Analytical-Based Lightning-Induced Damage Model for an Aircraft Wing Exposed to Pressure Loading of Lightning;Mathematical Problems in Engineering;2024-01-27

4. Non-probabilistic credible reliability analysis of the composite laminate;Aerospace Science and Technology;2024-01

5. Impact of standard and unexpected bolt-hole-washer tolerances on the performance of pinned and torqued joints in CFRP composites;Alexandria Engineering Journal;2023-10

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