ANALYTICAL AND FINITE ELEMENT BUCKLING AND POST BUCKLING ANALYSIS OF LAMINATED PLATES

This examination is engaged into assessing the clasping heap of isotropic and overlaid plates (15o /3oo /45o /6oo ) which is exposed to in plane pressure. The investigation device utilized for this intention was ANSYS 19.0. The clasping load is assessed by changing the parameters, for example, angle proportion (a/b), thickness proportion (S) and limit conditions. It was noticed that diverse length to broadness proportion influenced the basic clasping load and the fiber direction edges likewise influenced the basic clasping load symmetric point employ plates.