Shell Element Orthotropic

Orthotropic materials have three mutually perpendicular planes of elastic symmetry.

Modulus of Elasticity – Longitudinal (E1)

Modulus of elasticity in the longitudinal direction. It also defined as the fiber direction or 1-direction.

Modulus of Elasticity – Lateral (E2)

Modulus of elasticity in lateral direction. It also defined as the matrix direction or 2-direction.

Poisson’s Ratio (NU12)

The ratio of lateral strain to longitudinal strain.

G12

In-plane shear modulus.

G1Z

Transverse shear modulus in the 1-Z plane.

G2Z

Transverse shear modulus for shear in the 2-Z plane.

Mass Density (RHO)

The density of a material is its weight per unit volume (in SI units).

Thermal Expansion Coefficient (Ai)

Thermal expansion coefficient in the i direction. (Real)

Reference Temperature (TREF)

The reference temperature for the calculation of thermal loads or a temperature dependent thermal expansion coefficient.

Xt and Xc

Allowable stresses or strains in tension and compression, respectively, in the longitudinal direction. These values are required if a failure index is desired.

Yt and Yc

Allowable stresses or strains in tension and compression, respectively, in the lateral direction. These values are required if a failure index is desired.

S

Allowable stress or strain for in-plane shear.

Structural Damping Coefficient (GE)

This value is found by multiplying the critical damping ratio C/C0 by 2.0.

F12

Interaction term in the tensor polynomial theory of Tsai-Wu. Required if the failure index by the Tsai-Wu theory is desired and if the value of F12 is different from 0.0.

STRN

For the maximum strain theory only. It indicates whether Xt, Xc, Yt, Yc and S are stress or strain allowable. (Real = 1.0, strain allowable; blank for stress allowable)