A Note on a Non-Linear Theory on Bending of Orthotropic Sandwich Plates
- 1 May 1968
- journal article
- research article
- Published by Cambridge University Press (CUP) in Aeronautical Quarterly
- Vol. 19 (2) , 127-134
- https://doi.org/10.1017/s0001925900004522
Abstract
Summary: The derivation of a non-linear theory on bending of orthotropic sandwich plates is carried out by the principle of complementary energy from elasticity. The governing differential equations and natural boundary conditions are obtained. The assumptions used are, namely, the facings are orthotropic thin elastic plates with negligible bending rigidities and are made of the same material; the orthotropic core can take the transverse shear only; and the transverse shortening of the core may be ignored. The geometrical non-linearities are equivalent to von Kármán’s theory for single-layered plates. Through the introduction of a “shear function”, the number of differential equations is reduced to three and the equations are in rather simple form. It appears that the equations obtained here would require, comparatively, the least amount of work for analysing the finite deflection sandwich plate problems having a wide range of properties of practical interest.Keywords
This publication has 4 references indexed in Scilit:
- General theory of sandwich plates with dissimilar facingsInternational Journal of Solids and Structures, 1965
- On the theory of sandwich panels in the reference stateInternational Journal of Engineering Science, 1965
- Errata-"Finite Deflections of Sandwich PlatesJournal of the Aeronautical Sciences, 1950
- Finite Deflections of Sandwich PlatesJournal of the Aeronautical Sciences, 1948