2015
DOI: 10.1016/j.compstruct.2014.08.005
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Stress and strain recovery for functionally graded free-form and doubly-curved sandwich shells using higher-order equivalent single layer theory

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Cited by 225 publications
(79 citation statements)
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“…A hybrid method composed of the layerwise theory, DQM, and Fourier series expansion was developed by Selahi et al (2014) for transient analysis of FGM truncated conical shells with variable thickness, under asymmetric dynamic pressures. Tornabene et al (2015) investigated recovery of the static transverse normal and shear stresses in FGM doubly-curved sandwich shells of revolution using Carrera's unified formulation and the DQM. Using the FSDT and dividing the FGM shell into homogeneous disks, and using the finite element method, Zamani Nejad (2015) performed elastic analysis of rotating axially graded truncated conical shells under non-uniform pressures.…”
Section: Introductionmentioning
confidence: 99%
“…A hybrid method composed of the layerwise theory, DQM, and Fourier series expansion was developed by Selahi et al (2014) for transient analysis of FGM truncated conical shells with variable thickness, under asymmetric dynamic pressures. Tornabene et al (2015) investigated recovery of the static transverse normal and shear stresses in FGM doubly-curved sandwich shells of revolution using Carrera's unified formulation and the DQM. Using the FSDT and dividing the FGM shell into homogeneous disks, and using the finite element method, Zamani Nejad (2015) performed elastic analysis of rotating axially graded truncated conical shells under non-uniform pressures.…”
Section: Introductionmentioning
confidence: 99%
“…Ansari et al [44] applied the variational differential quadrature (VDQ) method to study the free vibration characteristic of embedded functionally graded carbon nanotubereinforced composite (FG-CNTRC) spherical shells having classical boundary condition resting on the elastic foundation. Tornabene et al [45] applied the generalized differential quadrature method [45][46][47][48][49][50][51][52][53][54][55][56][57][58][59][60] and Carrera unified formulation to study the effect of Carbon Nanotube (CNT) agglomeration on the free vibration of laminated composite doubly-curved shells and panels reinforced by CNTs.…”
Section: Introductionmentioning
confidence: 99%
“…Pradyumna and Bandyopadhyay [12] used the finite element method to study the free vibration of functionally graded curved panels with classical boundary conditions by using a higher-order shear deformation theory. Tornabene and his team [13][14][15][16][17][18][19][20][21][22][23][24][25][26][27][28][29][30] extended the generalized differential quadrature (GDQ) method for the free vibration analysis of functionally graded circular and parabolic panels and shells of revolution with classical boundary conditions. Other related research results with the layered composite parabolic and circular panels can be seen in Refs [31][32][33][34][35][36][37][38][39][40][41][42][43][44][45][46].…”
Section: Introductionmentioning
confidence: 99%