Degradation of mechanical properties of laminates with multi delaminations.
Date of Issue2003
School of Mechanical and Aerospace Engineering
This report present a numerical model for rapidly computing the critical loads of beams with multiple delaminations and to analysis the buckling behaviour of laminated composite beam under in-place compression. This study is focused on beam has two unequal length parallel delaminations with one enveloping the other.
DRNTU::Engineering::Mechanical engineering::Mechanics and dynamics
Nanyang Technological University