๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

Thermally induced buckling of laminated composites by a layerwise theory

โœ Scribed by Jaehong Lee


Publisher
Elsevier Science
Year
1997
Tongue
English
Weight
508 KB
Volume
65
Category
Article
ISSN
0045-7949

No coin nor oath required. For personal study only.

โœฆ Synopsis


Thermal buckling analysis of laminated composites is presented by using a layer-wise theory. Governing buckling equations are derived from the variational principle and a finite element method is developed to formulate the problem. Numerical results are obtained and compared with those of other theories addressing the effects of the thickness-to-span ratio, lamination angle, the ratio of thermal expansion coefficients and degree of orthotropy on buckling temperature for antisymmetric angle-ply laminates. It is found that a layer-wise approach may be necessary for more accurate thermal buckling analysis of laminated composites.


๐Ÿ“œ SIMILAR VOLUMES


Modelling of composite and sandwich plat
โœ C.M.C. Roque; A.J.M. Ferreira; R.M.N. Jorge ๐Ÿ“‚ Article ๐Ÿ“… 2005 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 281 KB

In this paper we use a trigonometric layerwise deformation theory for modelling symmetric composite plates. We use a meshless discretization method based on global multiquadric radial basis functions. The results obtained are compared with solutions derived from other models and numerical techniques

An adaptive enhancement of dynamic buckl
โœ Jinquan Cheng; Haipeng Han; Farid Taheri ๐Ÿ“‚ Article ๐Ÿ“… 2008 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 802 KB

A smart enhancement of dynamic buckling capacity of a laminated composite beam under an axial impact was achieved through surface bonded piezoelectric patches. It was demonstrated that applying the adaptive control of the electric field to the surface bonded piezoelectric patch could significantly d