Complementary energy theorem for thin composite plates in postbuckling

Capa

Citar

Texto integral

Acesso aberto Acesso aberto
Acesso é fechado Acesso está concedido
Acesso é fechado Somente assinantes

Resumo

The thin composite von Kármán plates in postbuckling are considered. Using the first Piola stress tensor and the displacement gradient tensor, the complementary energy variational theorem is proven. The Kirchhoff assumptions are adopted. The plate lay-up is symmetric and pointwise. According to the theorem, at the actual stress state of the plate the complementary energy (as a functional of the internal forces and of the moments) reaches its stationary value. The stationary feature of the actual state is valid as compared to other feasible states satisfying the static equilibrium and the static boundary conditions. The theorem is a consent of the static variational principle. The principle leads to the linear relations between forces/moments, created by the corresponding first Piola stress tensor components, and the 2D-strains/curvatures. An illustrative plate example is given.

Sobre autores

S. Selyugin

Department of Airplane Design and Certification, Moscow Aviation Institute (National Research University)

Autor responsável pela correspondência
Email: selyuginSV@mai.ru
Rússia, Moscow

Bibliografia

  1. Turvey G.J., Marshall I.H., eds. Buckling and Postbuckling of Composite Plates. Chapman and Hall, 1995. https://doi.org/10.1007/978-94-011-1228-4
  2. Falzon BG, Aliabadi MH, eds. Buckling and postbuckling structures, volume 1. Imperial College Press, 2008. https://doi.org/10.1142/p506
  3. Xu J., Zhao Q., Qiao P. A critical review on buckling and post-buckling analysis of composite structures // Frontiers in Aerospace Engineering. 2013. № 2. P. 157–168.
  4. Grishin V.I., ed. Design, analysis and static tests of metallic-composite structures (in Russian). Moscow: Technosfera, 2022.
  5. Azikov N.S., Zinin A.V., Gaidarzhi U.V., Saifullin I.S. Strength of skewed composite panels in postbuckling // Machine-building and machine-reliability problems. 2021. № 5. P. 62–71.
  6. Mitrofanov O., Osman M. Designing of smooth composite panels providing stability and strength at postbuckling behavior // Mech Compos Mater. 2022. V. 58. P. 15–30. https://doi.org/10.1007/s11029-022-10008-3
  7. Wu Z., Raju G., Weaver P.M. Postbuckling analysis of variable angle tow composite plates // Int. J. Solids Struct. 2013. V. 50. P. 1770–1780. https://doi.org/10.1016/j.ijsolstr.2013.02.00
  8. Washizu K. Variational methods in elasticity and plasticity. 3rd edition. Pergamon Press, 1982.
  9. Novozhilov V.V. Theory of elasticity (in Russian). Leningrad: Sudpromgiz, 1958.
  10. Stumpf H. Die Extremalprinzipe der nichtlinearen Plattentheorie // ZAMM. 1975. № 55. P. 110–112.
  11. Wang C.-T. Principle and application of complementary energy method for thin homogenious and sandwich plates and shells with finite deflections. NACA TN 2620, 1952.
  12. Reddy J.N. Mechanics of laminated composite plates and shells. Theory and analysis. 2nd edition. Taylor and Francis, Inc., 2003. 831 p. https://doi.org/10.1201/b12409
  13. Ashton J.E., Whitney J.M. Theory of laminated plates. Technomic Publ. 1970.
  14. Vasilyev VV. Mechanics of structures made of composite materials (in Russian). Mashinostroenie. 1988.
  15. Gibson R.F. Principles of composite material mechanics. 4th edition. Taylor and Francis, Inc., 2016. 425 p. https://doi.org/10.1201/b19626

Arquivos suplementares

Arquivos suplementares
Ação
1. JATS XML

Declaração de direitos autorais © Russian Academy of Sciences, 2024