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Laminate Composites > Laminates theory > First order shear deformation theory

Constitutive equations

The equations are written in the 12 (ply) coordinate system, in which the ply material properties are defined. In this local coordinate system, the stress-strain relationship can be written:

where:

  • E1 is Young’s modulus in 1-direction

  • E2 is Young’s modulus in 2-direction,

  • G12 is the shear modulus in the 12 plane,

  • ν12 is the major Poisson’s ratio,

  • ν21 is the minor Poisson’s ratio,

Transverse stresses can be related to transverse strains with the following equation:

where G13 and G23 correspond to the transverse shear moduli.

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First order shear deformation theory

Strain displacement relationship

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Shell stress resultants

Laminate stiffness matrices

Transverse shear stiffness matrix

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Constitutive equations, Simcenter 3D 2021.1 Series

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Source: https://docs.sw.siemens.com/en-US/doc/289054037/PL20200601120302950.advanced/id626711 · retrieved 2026-07-17