GENERAL EQUATIONS OF ANISOTROPIC PLATES AND SHELLS INCLUDING TRANSVERSE SHEAR DEFORMATIONS, ROTARY INERTIA AND INITIAL CURVATURE EFFECTS

By M. Toorani, A. Lakis. 2000

155 citations recorded by the source corpus.

Subfields: Control and Systems Engineering, Mechanical Engineering, Mechanics of Materials

View Paper: https://www.semanticscholar.org/paper/c995bd8f26571a601b65641d3ee43710500cdb66

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Control and Systems Engineering

In Mechanical Engineering

In Mechanics of Materials

Citations in the corpus

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): “In order to include the effect of the initial curvature in the evaluation of the stress resultants a generalization of the Classical Reissner–Mindlin Theory (CRMT) has been proposed in literature by Kraus [7], Qatu [16–18] and Toorani and Lakis [19].”
FREE VIBRATIONS OF FOUR-PARAMETER FUNCTIONALLY GRADED PARABOLIC PANELS AND SHELLS OF REVOLUTION (2009, background): “We notice that, in the above definitions (3) the symmetry of shearing force resultants ,s sN Nϕ ϕ and torsional couples ,s sM Mϕ ϕ is assumed as a further hypothesis, even if it is satisfied only in the case of spherical shells and flat plates (Toorani and Lakis, 2000).”
Free vibration analysis of functionally graded panels and shells of revolution (2009, background): “We notice that, in the above definitions (8) the symmetry of shearing force resultants Nϕs, Nsϕ and torsional couples Mϕs, Msϕ is assumed as a further hypothesis, even if it is satisfied only in the case of spherical shells and flat plates (Toorani and Lakis [ 37 ]).”
A unified formulation for vibration analysis of composite laminated shells of revolution including shear deformation and rotary inertia (2013, background): “This factor depends, in general, on the shell lamination parameters, such as number of layers, stacking sequence, degree of orthotropy and fiber orientation in each individual layer, the loading and boundary conditions [3].”
Mixed Static and Dynamic Optimization of Four-Parameter Functionally Graded Completely Doubly Curved and Degenerate Shells and Panels Using GDQ Method (2013, methodology): “[21] M. H. Toorani and A. A. Lakis, “Free vibrations of non-uniform composite cylindrical shells,” Nuclear Engineering and Design, vol. 236, no. 17, pp. 1748–1758, 2006.”