Static analysis of laminated composite curved shells and panels of revolution with a posteriori shear and normal stress recovery using generalized differential quadrature method

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Static analysis of functionally graded conical shells and panels using the generalized unconstrained third order theory coupled with the stress recovery (2014, methodology): “With the in-plane stress components indirectly derived from the GDQ-solution [54–92] of the fundamental system, the integration of the three dimensional indefinite equilibrium equations is carried out.”
Four-parameter functionally graded cracked plates of arbitrary shape: A GDQFEM solution for free vibrations (2016, unknown): “It appears from several papers in the literature that this numerical approach has been widely used in the past [24–39].”
Static analysis of doubly-curved anisotropic shells and panels using CUF approach, differential geometry and differential quadrature method (2014, background): “In order to satisfy the boundary conditions s13ðijIT Þ 1⁄4 q ðþÞ 1ðijÞ; s23ðijIT Þ 1⁄4 q ðþÞ 2ðijÞ the corresponding profiles have to be corrected [59,87,88,90,95,98] in the following manner s13ðijmÞ 1⁄4 s13ðijmÞ þ q 1ðijÞ s13ðijIT Þ h fðmÞ þ h 2 m 1⁄4 1; .”