4.7 Article

Assessment of zigzag theory for static loading, buckling, free and forced response of composite and sandwich beams

Journal

COMPOSITE STRUCTURES
Volume 64, Issue 3-4, Pages 317-327

Publisher

ELSEVIER SCI LTD
DOI: 10.1016/j.compstruct.2003.08.013

Keywords

laminates; vibration; buckling; analytical modelling

Ask authors/readers for more resources

An efficient zigzag one-dimensional (1D) theory of laminated beams is assessed by comparison of analytical solutions of simply supported beam with exact 2D elasticity solutions for static patch load, natural frequencies, harmonic transverse load with sinusoidal longitudinal variation and buckling under axial load. These results for a highly inhomogeneous test beam, symmetric composite beam, anti-symmetric composite beam and sandwich beam are also compared with first order (FSDT) and third order (TOT) shear deformation theories. The effect of the laminate lay-up and the thickness-to-span ratio on the accuracy is assessed. The zigzag theory yields much more accurate results than the TOT and FSDT. (C) 2003 Elsevier Ltd. All rights reserved.

Authors

I am an author on this paper
Click your name to claim this paper and add it to your profile.

Reviews

Primary Rating

4.7
Not enough ratings

Secondary Ratings

Novelty
-
Significance
-
Scientific rigor
-
Rate this paper

Recommended

No Data Available
No Data Available