MITC finite elements for laminated composite plates

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FREE VIBRATIONS OF FOUR-PARAMETER FUNCTIONALLY GRADED PARABOLIC PANELS AND SHELLS OF REVOLUTION (2009, background): “In particular, it is worth noting that the determination of shear correction factors for composite laminated structures is still an unsolved issue, because these factors depend on various parameters (Alfano et al., 2001; Auricchio and Sacco, 1999, 2003).”
Static analysis of laminated composite curved shells and panels of revolution with a posteriori shear and normal stress recovery using generalized differential quadrature method (2012, methodology): “The finite element method do not present these drawbacks and it represents the most popular numerical tool in carrying out the above analyses [14,15,21,26–29].”
Free vibration analysis of functionally graded conical, cylindrical shell and annular plate structures with a four-parameter power-law distribution (2009, background): “In particular, it is worth noting that the determination of shear correction factors for composite laminated structures is still an unresolved issue, because these factors depend on various parameters [56–58]).”
Free vibration analysis of functionally graded panels and shells of revolution (2009, unknown): “[34], Auricchio and Sacco [35, 36]).”