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@article{176997,
        author = {Jagadish R Bagali},
        title = {INFLUENCE OF A LINEARLY VARIABLE IN-PLANE LOAD ON THE BUCKLING OF SYMMETRICAL CROSS-PLY COMPOSITE RECTANGULAR PLATES},
        journal = {International Journal of Innovative Research in Technology},
        year = {2025},
        volume = {1},
        number = {6},
        pages = {2161-2166},
        issn = {2349-6002},
        url = {https://ijirt.org/article?manuscript=176997},
        abstract = {The purpose of this article is to present a solution in order to provide a precise solution for the buckling of simply supported symmetrical cross-ply composite rectangular plates that are exposed to a linearly varying edge stress. This article's objective is to offer a solution. During its development, the theory of shear deformation of the first order served as the basis for its application, and it was used on laminated plates that had a thickness that was quite low. The purpose of this investigation is to ascertain the buckling loads of cross-ply rectangular plates that have a variety of aspect ratios that are distinct from one another. On top of that, the effects of altering the intensity of the load as well as the arrangement of the layup on the buckling load are investigated. A piece of software known as ABAQUS is used on the computer in order to achieve the objective of ensuring that the results are accurate.},
        keywords = {In-plane Load, Buckling, Cross ply, Composite Plate.},
        month = {April},
        }