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Title of Journal: Int Appl Mech

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Abbravation: International Applied Mechanics

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Springer US

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DOI

10.1007/s11569-011-0113-3

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1573-8582

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Stability of composite shells of revolution

Authors: V M Trach
Publish Date: 2008/08/05
Volume: 44, Issue: 3, Pages: 331-344
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Abstract

An approach to solving the buckling problem for shells made of a composite material with one plane of elastic symmetry is presented The approach employs complex Fourier series The prebuckling stressstrain state is assumed to be geometrically nonlinear The stability of a cylindrical shell under axial compression and uniform side pressure is analyzed using the RungeKutta method with discrete orthogonalization The numerical results are compared with analytical solutions

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Other Papers In This Journal:
  1. Forced Monoharmonic Vibrations and Self-Heating of Viscoelastic Flexible Circular Plates with Piezoelectric Layers
  2. Stability of the Horizontal Flight of an Aircraft
  3. Vibration Modes of Radially Polarized Thin Cylindrical Piezoceramic Rings
  4. Practical Stability of a Moving Robot with Respect to Given Domains
  5. Identification of nonstationary axisymmetric load distributed along a cylindrical shell
  6. Linearization of dynamic equations for a saturated porous medium
  7. Stability of composite materials with two parallel short fibers
  8. Stability of composite materials with two parallel short fibers
  9. Parametric stability of singularly perturbed nonlinear uncertain systems
  10. Spatial Problems of the Fracture of Materials Loaded Along Cracks (Review)
  11. Distribution of Contact Pressure Between a Sealing Element and a Cylinder
  12. Rayleigh wave in a quadratic nonlinear elastic half-space (Murnaghan model)
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