Linear and Nonlinear Stability Analysis of Thin Rectangular Plates Subjected to Local In-Plane Shearing-Reference-Cited by-同舟云学术

Linear and Nonlinear Stability Analysis of Thin Rectangular Plates Subjected to Local In-Plane Shearing

Published:2023-07-07 Issue:4 Volume:33 Page:689-698
ISSN:1016-8664
Container-title:Structural Engineering International
language:en
Short-container-title:Structural Engineering International

Author:

Kacimi Amar¹^ORCID,Ikhenazen Ghania¹^ORCID,Mohri Foudil²^ORCID,Saidani Messaoud³^ORCID,Kilardj Madina⁴

Affiliation:

1. the Built Environment Research Laboratory (LBE), Faculty of Civil Engineering, University of Sciences and Technology H. Boumediene, Algiers, Algeria

2. Laboratoire d’Etude des Microstructures et de Mécanique des Matériaux (LEM3), Université de Lorraine, Metz, France

3. Research Institute of Clean Growth and Future Mobility, Coventry University, Coventry, England, United Kingdom

4. the Built Environment Research Laboratory (LBE), Dr, Faculty of Civil Engineering, University of Sciences and Technology H. Boumediene, Algiers, Algeria

Publisher

Informa UK Limited

Subject

Building and Construction,Civil and Structural Engineering

Link

https://www.tandfonline.com/doi/pdf/10.1080/10168664.2023.2208143

Reference44 articles.

1. Essai théorique sur les vibrations des plaques élastiques, rectangulaires et libres;Bernoulli JI.;Nova Acta Acad. Sci. Imp. Petrop,1789

2. Navier C. Bulletin des Sciences de la Société Philomathique de Paris. In Paris. 1823.

3. Über das Gleichgewicht und die Bewegung einer elastischen Scheibe.

4. On the stability under shearing forces of a flat elastic strip;Southwell RV;Proc. Math. Phys,1924

5. Stein M, Neff J. Buckling stresses of simply supported rectangular flat plates in shear. In. National Aeronautics and Space Admin Langley Research Centre, Hampton, VA: National Advisory Committee Buckling For Aeronautics. 1974.