This review paper focuses on structural optimization and dynamic characterization of Nanoclay reinforced laminated plates made up of hybrid composites. By using shear deformation theory with higher order which bounds within a method of finite element formulation for surveys, such a governing differential equations of motion for such plates as well have been justified. The study aims to highlight the properties of composite plates like stiffness and damping which are crucially varies with different percentage of Nanoclay reinforced and different Nanoclay aspect ratios. As well, discussions have been done which gone through the finite element method upon comparing the natural frequencies in experimental results in variety of literatures. Additionally, the exploration effects of Nanoclay aspect ratios, Ply onboarding, Nanoclay, bounding conditions on the natural frequencies, and Nanoclay reinforced composite plate’s mode shapes are conducted by the way various parametric studies. Small fly configuration aspect ratios are identified by the research and formulating multi-objective optimization identifies the Nanoclay volume fraction. These issues are mainly aimed at reducing the modal damping factors and stiffness of the composite plates. Also, this research highlights the importance of Nanoclay reinforcement with the results offering valuable guidelines for designing the structures of hybrid composite plates used in aerospace and automobile applications. Likewise, study also focuses and shows the use of reference for the fibre-reinforced plastics to apply various devices and structures like various field components including automotive industries and aerospace, bicycle helmets, wind turbines, spacecraft, space elevator and solar panels.