1. Additions of optimal nanoparticles of SiO2 into APC-2 cross-ply laminates were used to improve the mechanical properties of hybrid laminates even at elevated temperature.

2. Numerical results are given for cross-ply plates and panels under S4S4 and S4S2 boundary conditions.

3. The large deflection problems of the symmetrically laminated cross-ply circular plates of fiber reinforced composites are investigated in this paper by using Galerkins procedure.

4. In this paper, axisymmetric nonlinear dynamic equations of fiber reinforced symmetric cross-ply laminated flat spherical shells are found including transverse shear deformation.

5. The Rayleigh-Ritz method is used to calculate the critical load at which delamination buckling will occur for a symmetric cross-ply composite laminate containing a single delamination.

6. Combining with the experiences of design and practice in our factory, in this paper, an extensive and intensive investigation was made in diversiform cross-ply tire molds of the factory.

7. Transverse cracking of matrix is a main damage type of cross-ply laminates.

8. The delamination is assumed to be elliptical in shape. In this paper the critical load of delamination buckling for a symmetric cross-ply laminate acted on by biaxial load is investigated.

9. In this paper the critical load of delamination buckling for a symmetric cross-ply laminate acted on by uniaxial load is investigated.

10. The characteristics of electric resistance-strain relationship of unidirectional and cross-ply CFRP laminates were studied under static and tensile-tensile dynamic loading.

11. Furthermore, it indicates that it is suitable to analyse the ultimate load of a cross-ply laminated short beam with the measured shear strength of cross-interlamination.

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12. Based on the plane elasticity, a hybrid, state-space-based, differential quadrature method is presented for static analysis of cross-ply laminated beams.

13. The present results may provide an important theoretical basis for further studying the micro-failure mechanism, ultimate strength and synergistic effect for cross-ply laminates under tension.