Dynamic behaviour of perforated laminated panels under biaxial non-uniform edge loads based on FE approach
Author:
Publisher
Elsevier BV
Subject
General Medicine
Reference19 articles.
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2. Stability vibration of isotropic orthotropic and laminated plates according to a higher-order shear deformation theory;Reddy;J. Sound Vib.,1985
3. Stability and vibration of laminated plates by using a mixed element based on a refined plate theory;Putcha;J. Sound Vib.,1986
4. Vibration and buckling of a simply supported rectangular plate subjected to a pair of in-plane concentrated forces;Leissa;J. Sound Vib.,1988
5. Elastic stability of simply supported rectangular plates under locally distributed edge forces;Baker;J. Appl. Mech.,1982
Cited by 4 articles. 订阅此论文施引文献 订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献
1. Optimum arrangement of stiffener on the buckling behaviour of stiffened composite panels with reinforced elliptical cutouts subjected to non-uniform edge load;STEEL COMPOS STRUCT;2022
2. Effect of trapezoidal shapes and non-uniform edge loads on buckling behaviour of plates with cutouts;Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science;2022-02-16
3. Effect of nonlinear edge loads and hybridization of FMLs on buckling performance of interlaminar composites with/without cutouts;Proceedings of the Institution of Mechanical Engineers, Part C: Journal of Mechanical Engineering Science;2021-08-28
4. Influence of Trapezoidal Shapes and Linearly varying Edge Loads on the Buckling Characteristics of Plates with Cutouts;Journal of The Institution of Engineers (India): Series C;2021-07-17
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