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@article{182791,
        author = {Hosmani Goutamkumar and Rajashekar M},
        title = {BUCKLING LOAD FOR CROSS PLY SIMPLY SUPPORTED COMPOSITE PLATE FOR DIFFERENT ASPECT AND MODULI RATIOS UNDER BIAXIAL COMPRESSION},
        journal = {International Journal of Innovative Research in Technology},
        year = {2025},
        volume = {6},
        number = {6},
        pages = {231-236},
        issn = {2349-6002},
        url = {https://ijirt.org/article?manuscript=182791},
        abstract = {In order to investigate the buckling load in biaxially loaded rectangular laminated plates, a numerical technique is used. For the purpose of conducting buckling analysis on thin rectangular laminated plates within the framework of classical laminated plate theory (CLPT), a Fortran software that is based on finite elements (FE) has been created. An investigation has been conducted on the issue of buckling stresses of composite plates that are typically stacked. Analysis and resolution of the issue are accomplished by the use of the energy strategy, which is described by a finite element model. A model with four nodes is used in this approach, which involves the application of quadrilateral parts. At each node, there are three degrees of freedom for each individual constituent. As far as degrees of freedom are concerned, they are as follows: lateral displacement, rotation, and around the axes and correspondingly. Buckling loads are analyzed and verified with other works that are accessible in the literature in order to verify the correctness of the approach that is currently being performed. This indicates that the finite element approach that was employed is reliable since it has a good agreement with the data that is accessible.},
        keywords = {Finite element, Fortran program, Buckling load, Simply supported, Composite plate.},
        month = {July},
        }