Impact Analysis of Aluminum-Fibre Laminated Composite

Abstract:

Article Preview

Impact analysis of an advanced laminated composite comprising aerospace 2024-T3 aluminum alloy and resin impregnated E-glass fiber layers with different stacking sequences is presented in the paper. The panel under study is subjected to load-time history equivalent to the low velocity crash using FEM software ANSYS 12. Stress values in the laminate are found to be discontinuous at the interfaces whereas the displacements are continuous across the interfaces. The maximum stress and displacement values in the laminate are comparable with those in monolithic aluminum alloy panel of same thickness.

Info:

Periodical:

Advanced Materials Research (Volumes 311-313)

Edited by:

Zhongning Guo

Pages:

309-313

DOI:

10.4028/www.scientific.net/AMR.311-313.309

Citation:

P. Sharma et al., "Impact Analysis of Aluminum-Fibre Laminated Composite", Advanced Materials Research, Vols. 311-313, pp. 309-313, 2011

Online since:

August 2011

Export:

Price:

$35.00

In order to see related information, you need to Login.

In order to see related information, you need to Login.