Abstract Views :132 |
PDF Views:0
Authors
Affiliations
1 Department of Applied Mechanics, Maulana Azad National Institute of Technology, Bhopal, IN
Source
International Journal of Scientific Engineering and Technology, Vol 1, No 4 (2012), Pagination: 93-95
Abstract
The effect of fibre orientation on buckling behaviour in a rectangular composite laminate with central circular hole under uniform in-plane loading has been studied by using finite element method. The critical buckling loads with different fibre orientation in an orthotropic composite laminate (E-glass/epoxy) were obtained. The deformation behaviour of the plate is shown for modes, i=1,2. Studies are carried out for three D/A ratio (where D is hole diameter and A is plate width) with different plate thickness (number of layers). The finite element formulation is carried out in the analysis section of the ANSYS software.
Keywords
Orthotropic Composite Laminates, Fibre Orientation, Buckling Analysis, Eigen Value, ANSYS.
Full Text
