2013
DOI: 10.1016/j.compositesb.2012.09.043
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Elastic analysis of pressurized thick cylindrical shells with variable thickness made of functionally graded materials

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Cited by 72 publications
(28 citation statements)
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“…Abediokhchi et al (2013) presented a bending analysis for the FGM conical panels based on the FSDT and generalized differential quadrature (GDQ) solution method. The FSDT and the perturbation theory were employed by Ghannad et al (2013) for deformation and stress analysis of axisymmetric clamped variable thickness FGM cylindrical shells under internal pressures. Tornabene et al (2013) applied the GDQ Method, FSDT, and stress recovery approach for stress analysis of transversely graded and laminated composite shells of revolution.…”
Section: Introductionmentioning
confidence: 99%
“…Abediokhchi et al (2013) presented a bending analysis for the FGM conical panels based on the FSDT and generalized differential quadrature (GDQ) solution method. The FSDT and the perturbation theory were employed by Ghannad et al (2013) for deformation and stress analysis of axisymmetric clamped variable thickness FGM cylindrical shells under internal pressures. Tornabene et al (2013) applied the GDQ Method, FSDT, and stress recovery approach for stress analysis of transversely graded and laminated composite shells of revolution.…”
Section: Introductionmentioning
confidence: 99%
“…Thus, applying the rule of mixture (13) first to the coefficient of thermal expansion α(r) and then also to the density ρ(r), the uniaxial yield limit σ y (r), and the thermal conductivity k(r) one obtains P r eff (r) = A P r r a m + B P r (17) with…”
Section: Governing Equationsmentioning
confidence: 99%
“…Now, the governing equations for the FGM-panel can be derived. First, using (12), (15), (17), and (18), the axial stress can be expressed by…”
Section: Governing Equationsmentioning
confidence: 99%
“…They assumed a realistic parabolic variation of transverse shear strains through the shell thickness and considered Sander's approximations to include the effect of three curvature terms in the strain components of composite shells. Ghannad et al (2013) presented a closed form analytical solution for clamped-clamped thick cylindrical shells with variable thickness made of functionally graded materials subjected to constant internal pressure based on FSDT.…”
Section: Introductionmentioning
confidence: 99%