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In this work, a new composite sandwich plate including a viscoelastic material (VEM) filling orthogrid core is proposed. Taking temperature and moisture effects into consideration, the dynamic ‘analysis for impact responses of this structure is presented. The equivalent material properties of the composite core layer are calculated using the Halpin–Tsai model. In order to model the impact force between the impactor and the structure, the modified Hertz contact law is utilized. The governing equations of the structure are derived by employing the Reddy’s higher-order shear deformation theory (HSDT) and Hamilton’s principle. Then the governing equations are solved through the Galerkin method with the aid of the Newmark direct integration scheme. After verifying the reliability and accuracy of this model, the effects of temperature, moisture, initial velocity of the impactor and boundary condition on the contact force and central deflection of the structure are discussed in detail. It has been demonstrated that changes of environmental temperature and moisture play a significant effect on the damping characteristics and impact responses of the composite sandwich plates.

The present paper aims to investigate the buckling load of functionally graded carbon-fiber-reinforced polymer (FG-CFRP) composite laminated plates under in-plane loads in a thermal environment. The effective material properties of the CFRP composite are calculated by the Mori–Tanaka homogenization method. The theoretical formulations are based on classical laminate plate theory (CLPT) and the von Kármán equations for large deflections. The governing equations are derived based on the principle of virtual work and then solved through the Navier solution. Results are obtained for the critical buckling load and temperature effect of a simply supported plate subjected to in-plane loading. A detailed numerical study is conducted to provide important insights into the effects of the functionally graded carbon fiber (CF) distribution pattern and volume fraction, total number of layers, temperature, geometrical dimension and lamination angle on the buckling load of functionally carbon-fiber-reinforced composite plates. Finally, the validation is compared with the Reddy and finite element analyses, which show consistency with each other.

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