The postbuckling behaviour of adhesively bonded stiffened panels subjected to in-plane shear loading-Reference-Cited by-同舟云学术

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The postbuckling behaviour of adhesively bonded stiffened panels subjected to in-plane shear loading

Published:2015-10 Issue: Volume:46 Page:30-41
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

de Paula Guedes Villani Anaisa^ORCID,Donadon Mauricio V.,Arbelo Mariano A.,Rizzi Paulo,Montestruque Carlos V.,Bussamra Flavio,Rodrigues Marcelo R.B.

Funder

CNPq

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference28 articles.

1. Static and fatigue testing thin riveted, bonded and hybrid carbon fiber double lap joints used in aircraft structures;Chowdhury;Compos. Struct.,2015

2. Fatigue threshold behavior of adhesive joints;Azari;Int. J. Adhes. Adhes.,2010

3. Thermal post-buckling behaviour of laminated composite cylindrical/hyperboloidal shallow shell panel using nonlinear finite element method;Panda;Compos. Struct.,2009

4. Post-buckling analysis of laminated composite doubly curved panel embedded with SMA fibres subjected to thermal environment;Panda;Mech. Adv. Mat. Struct.,2013

5. Thermal post-buckling analysis of laminated composite shell panel using NFEM;Panda;Mech. Based Des. Struct. Mach.,2013

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2. Prediction method for shear stability of composite hat-stringer stiffened panel;Aerospace Systems;2023-04-28

3. Ratcheting characterization and its effect on low cycle fatigue behavior of DP600 steel sheet under cyclic shear path;International Journal of Fatigue;2023-01

4. Experimental behavior and shear bearing capacity simulation of stiffened composite panels subjected to invisible damage impact;Thin-Walled Structures;2022-09

5. A semi-analytical model for shear buckling analysis of stiffened composite panel with debonding defect;Thin-Walled Structures;2022-02

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