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@article{182917,
        author = {Chandrashekharaiah S B and Ananda C B and Mamatha A},
        title = {BUCKING LOAD ON A SIMPLY SUPPORTED COMPOSITE PLATE USING BIAXIAL COMPRESSION FOR VARIOUS ASPECTS AND MODULE RATIOS},
        journal = {International Journal of Innovative Research in Technology},
        year = {2025},
        volume = {9},
        number = {9},
        pages = {828-833},
        issn = {2349-6002},
        url = {https://ijirt.org/article?manuscript=182917},
        abstract = {The usage of a numerical approach is performed in order to examine the buckling load in rectangular laminated plates that are loaded in a biaxial direction. A Fortran program that is based on finite elements (FE) has been developed for the purpose of performing buckling analysis on thin rectangular laminated plates within the framework of classical laminated plate theory (CLPT). This was done in order to fulfill the objective of doing the analysis. Buckling stresses of composite plates that are generally stacked have been the subject of research that has been carried out. The use of the energy strategy, which is characterized by a finite element model, is what allows for the analysis and resolution of the problem. This method, which includes the use of quadrilateral components, makes use of a model that consists of four nodes. There are three degrees of freedom for each unique element at each node in the network. When it comes to degrees of freedom, the following are the degrees of freedom that are involved: rotation, lateral displacement, and rotation around the axes, and similarly. The technique that is now being carried out is subjected to analysis and verification with other works that are available in the literature. This is done in order to ensure that the approach is accurate. This demonstrates that the finite element method that was used is trustworthy since it has a high degree of concordance with the data that is not just available but also readily available.},
        keywords = {Finite element, Fortran program, Buckling load, Simply supported, Composite plate.},
        month = {July},
        }