Article ID | Journal | Published Year | Pages | File Type |
---|---|---|---|---|
5028344 | Procedia Engineering | 2017 | 8 Pages |
Abstract
Nonlinear response of laminated composite plates and cylindrical panels subjected to a parabolically distributed blast load is studied here using a shear deformable finite element method. The nonlinear finite element equations of motion are solved in the time domain by an energy and momentum conserving time integration technique. The state-of-stress inside the laminated panels is calculated at each time-step to predict the occurrence of damage using Tsai-Wu quadratic failure criterion. The effects of span-to-thickness ratio, radius-to-span ratio and peak pressure on the nonlinear dynamic response of laminated composite plates and curved panels are investigated.
Related Topics
Physical Sciences and Engineering
Engineering
Engineering (General)
Authors
Emarti Kumari, M.K. Singha,