Experimental and Numerical Post-buckling Analysis of Thin Aluminium Aeronautical Panels under Shear Load-Reference-Cited by-同舟云学术

Experimental and Numerical Post-buckling Analysis of Thin Aluminium Aeronautical Panels under Shear Load

Published:2014-01-22 Issue:3 Volume:50 Page:208-222
ISSN:0039-2103
Container-title:Strain
language:en
Short-container-title:Strain

Author:

Cricrì G.¹,Perrella M.¹,Calì C.¹

Affiliation:

1. Department of Industrial Engineering; University of Salerno; Fisciano Italy

Publisher

Wiley

Subject

Mechanical Engineering,Mechanics of Materials

Link

http://onlinelibrary.wiley.com/wol1/doi/10.1111/str.12083/fullpdf

Reference14 articles.

1. Computational and experimental methods in structures;Kling,2008

2. Calì , C. Armentani , E. Caputo , Jr. F. Godono , G. 1999 Macchina per prove di pannellature aeronautiche sotto carichi multi assiali Proc. Natl. Conf. XXVIII AIAS

3. Numerical solution techniques for structural instability problems;Calì;J. Achiev. Mater. Manuf. Eng,2006

4. A finite element simulation of the test procedure of stiffened panels;Hu;Mar. Struct.,1998

5. The computational post-buckling analysis of fuselage stiffened panels loaded in compression;Lynch;Thin-Walled Struct.,2004

Cited by 11 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Numerical and experimental investigation of a metallic fuselage stiffened panel loaded with a representative fuselage fatigue spectrum;International Journal of Fatigue;2024-05

2. Stability of cruciform specimens for fracture tests under compression;Engineering Fracture Mechanics;2022-02

3. Experimental and Analytical Investigation of the Shear Fracture Behavior of Bonded Joints;Macromolecular Symposia;2021-04

4. Mode I Fracture Toughness Evaluation of Adhesively Bonded Joints via J‐Integral and DIC;Macromolecular Symposia;2020-02

5. A Continuation Procedure for the Quasi-Static Analysis of Materially and Geometrically Nonlinear Structural Problems;Mathematical and Computational Applications;2019-11-02