*SHELL GENERAL SECTION

Products Abaqus/Standard Abaqus/Explicit Abaqus/CAE

Type Model data

LevelPartPart instance

Abaqus/CAE Property module

Required parameters

ELSET: Set this parameter equal to the name of the element set containing the shell elements for which the section behavior is being defined.

Required parameter in Abaqus/Explicit, optional parameter in Abaqus/Standard

DENSITY

Set this parameter equal to the mass per unit surface area of the shell.

If the MATERIAL and COMPOSITE parameters are omitted, this density accounts for the mass of the shell, since no material definition is given.

If the MATERIAL or COMPOSITE parameter is used, the mass of the shell includes a contribution from this parameter in addition to any contribution from the material definition.

Optional parameters

BENDING ONLY

Include this parameter to ignore membrane stiffness effects in the shell. Bending stiffness and transverse shear stiffness coefficients are computed normally. Membrane-bending coupling coefficients are set to zero. Diagonal membrane stiffness coefficients are set to 1 × 10⁻⁶ times the largest diagonal bending stiffness term. Off-diagonal membrane stiffness coefficients are set to zero.

CONTROLS

In an Abaqus/Explicit analysis, set this parameter equal to the name of a section controls definition (see Section Controls) to be used to specify the second-order accurate element formulation option, a nondefault hourglass control formulation option, or scale factors.

In an Abaqus/Standard analysis, set this parameter equal to the name of a section controls definition to be used to specify the enhanced hourglass control formulation (see Section Controls) or to be used in a subsequent Abaqus/Explicit import analysis.

LAYUP

This parameter is relevant only when the COMPOSITE parameter is used.

Set this parameter equal to the name of a composite layup (see Composite layups). Abaqus/CAE uses this name to identify the composite layup that contains the shell section.

MEMBRANE ONLY

Include this parameter to ignore bending stiffness effects in the shell. Membrane stiffness and transverse shear stiffness coefficients are computed normally. Membrane-bending coupling coefficients are set to zero. Diagonal bending stiffness coefficients are set to 1 × 10⁻⁶ times the largest diagonal membrane stiffness term. Off-diagonal bending stiffness coefficients are set to zero.

OFFSET

Include this parameter to define the distance (as a fraction of the shell thickness) from the shell midsurface to the reference surface (containing the nodes of the element). This parameter accepts positive or negative values, the labels SPOS or SNEG, or in an Abaqus/Standard analysis the name of a distribution (see Distribution Definition).

Positive values of the offset are in the positive normal direction (see About Shell Elements). When OFFSET=0.5 (or SPOS), the top surface of the shell is the reference surface. When OFFSET=−0.5 (or SNEG), the bottom surface of the shell is the reference surface. The default is OFFSET=0, which indicates that the middle surface of the shell is the reference surface.

In an Abaqus/Standard analysis a spatially varying offset can be specified by setting OFFSET equal to the name of a distribution. The distribution used to define the shell offset must have a default value. The default offset is used by any shell element assigned to the shell section that is not specifically assigned a value in the distribution.

ORIENTATION

Set this parameter equal to the name of an orientation definition (see Orientations) to be used with the section forces and section strains.

POISSON

Include this parameter to define the shell thickness direction behavior.

Set this parameter equal to a nonzero value to cause the thickness direction strain under plane stress conditions to be a linear function of the membrane strains. The value of the POISSON parameter must be between −1.0 and 0.5.

Set POISSON=ELASTIC to automatically select this parameter value based on the initial isotropic elastic part of the material definition.

The default is POISSON=0.5.

SMEAR ALL LAYERS

This parameter is relevant only when the COMPOSITE parameter is used.

Include this parameter to ignore the material layer stacking sequence. Transverse shear stiffness coefficients are computed normally. Membrane-bending coupling terms are set to zero, and bending stiffness terms are computed as T²/12 times the corresponding membrane stiffness terms, where T is the total thickness of the shell.

STACK DIRECTION

This parameter is relevant only for continuum shells.

Set this parameter equal to 1, 2, 3, or ORIENTATION to define the continuum shell stack or thickness direction. Specify one of the numerical values to select the corresponding isoparametric direction of the element as the stack or thickness direction. The default is STACK DIRECTION=3.

If STACK DIRECTION=ORIENTATION, the ORIENTATION parameter is also required.

To obtain a desired thickness direction, the appropriate numerical value for the STACK DIRECTION parameter depends on the element connectivity. For a mesh-independent specification, use STACK DIRECTION=ORIENTATION. If the orientation assigned to the ORIENTATION parameter is defined with a distribution (Distribution Definition), STACK DIRECTION=ORIENTATION is not supported.

SYMMETRIC

This parameter is relevant only when the COMPOSITE parameter is used.

Include this parameter if the layers in the composite shell are symmetric about a central core. This parameter cannot be used if a spatially varying thickness or orientation angle is defined on any composite layer using a distribution (Distribution Definition).

THICKNESS MODULUS

This parameter is relevant only for continuum shells.

Set this parameter equal to the effective thickness modulus.

Set THICKNESS MODULUS=ELASTIC to compute the effective thickness modulus based on the in-plane elastic properties. In this case, the effective thickness modulus is set to the initial tensile modulus in the out-of-plane direction. If you use this option, you must define the shell thickness direction behavior using POISSON=ELASTIC.

ZERO

If the section is defined by its general stiffness, set this parameter equal to $θ^{0}$ , the reference temperature for thermal expansion (for example, ZERO=50 means $θ^{0} = 50^{\circ}$ ).

This parameter is ignored if the COMPOSITE, the MATERIAL, or the USER parameter is specified.

The following parameters are optional, mutually exclusive, and used only if the section is not defined by its general stiffness on the data lines

COMPOSITE

Include this parameter to indicate that the shell is composed of layers with different linear elastic material behavior.

MATERIAL

Set this parameter equal to the name of the single linear elastic material of which the shell is made.

USER

This parameter cannot be used with continuum shell elements. See Using a General Shell Section to Define the Section Behavior for use of this option in linear perturbation analyses.

Include this parameter to indicate that the shell section stiffness is defined in user subroutine UGENS (Abaqus/Standard) or user subroutine VUGENS (Abaqus/Explicit).

The following parameters are optional, mutually exclusive, and can be used only in combination with the MATERIAL, the COMPOSITE, or the USER parameter

NODAL THICKNESS

Include this parameter to indicate that the shell thickness should not be read from the data lines but should be interpolated from the thickness specified at the nodes with the NODAL THICKNESS option. For composite sections the total thickness is interpolated from the nodes, and the thicknesses of the layers specified on the data lines are scaled proportionally. This parameter is ignored for continuum shells.

SHELL THICKNESS

Set this parameter equal to the name of a distribution (Distribution Definition) to define spatially varying thickness. If this parameter is used for a non-composite section, the thickness on the data line is ignored. For composite sections the total thickness is defined by the distribution, and the thicknesses of the layers specified on the data lines are scaled proportionally. This parameter is ignored for continuum shells.

The distribution used to define shell thickness must have a default value. The default thickness is used by any shell element assigned to the shell section that is not specifically assigned a value in the distribution.

The following optional parameters can be used only in combination with the USER parameter

DELETE

This parameter applies only to Abaqus/Explicit analyses.

Set this parameter equal to the number of the solution-dependent variable (of those defined with the VARIABLES parameter) that controls the deletion of the element.

I PROPERTIES

Set this parameter equal to the number of integer property values needed as data in user subroutine UGENS or VUGENS. The default is I PROPERTIES=0.

PROPERTIES

Set this parameter equal to the number of real (floating point) property values needed as data in user subroutine UGENS or VUGENS. The default is PROPERTIES=0.

TVS DAMAGE

This parameter applies only to Abaqus/Explicit analyses.

Set this parameter equal to the number of the solution-dependent variable (of those defined with the VARIABLES parameter) that controls the transverse shear damage variable of the element.

UNSYMM

Include this parameter if the section stiffness matrices are not symmetric. This parameter will invoke the unsymmetric equation solution capability.

VARIABLES

Set this parameter equal to the number of solution-dependent variables that must be stored for the section. The default is VARIABLES=1.

Optional parameter for use when the MATERIAL, the COMPOSITE, and the USER parameters are omitted

DEPENDENCIES: Set this parameter equal to the number of field variable dependencies included in the definition of the scaling moduli, in addition to temperature. If this parameter is omitted, it is assumed that the moduli are constant or depend only on temperature.

Data line if the MATERIAL parameter is included

First (and only) line

Shell thickness. This value is ignored if the NODAL THICKNESS or SHELL THICKNESS parameter is included.

Data lines if the COMPOSITE parameter is included

First line

Positive scalar value defining layer thickness or the name of a distribution (Distribution Definition) that defines spatially varying layer thicknesses. A distribution for composite layer thickness can be used only for conventional shell elements (not continuum shell elements). The layer thickness is modified if the NODAL THICKNESS or SHELL THICKNESS parameter is included.
This field is not used (any value given will be ignored). It is included for compatibility with the SHELL SECTION option.
Name of the material forming this layer.
Orientation angle, $ϕ$ , or the name of a distribution (Distribution Definition) that defines spatially varying orientation angles. Orientation angles (in degrees) are measured positive counterclockwise relative to the orientation definition given with the ORIENTATION parameter. If the ORIENTATION parameter is not included, $ϕ$ is measured relative to the default shell local directions (see Conventions).
Name of the ply. Required only for composite layups defined in Abaqus/CAE.

Repeat this data line as often as necessary to define the layers of the shell. The order of the laminated shell layers with respect to the positive direction of the shell normal is defined by the order of the data lines. If the SYMMETRIC parameter is included, specify only half the layers, from the bottom layer to the midplane.

Data lines to define the shell section directly if the MATERIAL, the COMPOSITE, and the USER parameters are omitted

First line

Symmetric half of the $[D]$ matrix in the order $D_{11}$ , $D_{12}$ , $D_{22}$ , $D_{13}$ , $D_{23}$ , $D_{33}$ , $D_{14}$ ,..., $D_{44}$ , $D_{15}$ ,..., $D_{55}$ ,..., $D_{16}$ ,..., $D_{66}$

Repeat this data line three times. Enter 21 entries total, 8 per line on the first two lines and 5 on the third line.

Second line (optional)

${F}$ vector ( $F_{1}$ , $F_{2}$ , ..., $F_{6}$ ).

Third line (optional)

Y, scaling modulus for $[D]$ . The default is 1.0.
$α$ , scaling modulus for $[F]$ . The default is 0.0.
$θ$ , temperature for these values of Y and $α$ .
First field variable.
Second field variable.
Etc., up to five field variables.

Subsequent lines (only needed if the DEPENDENCIES parameter has a value greater than five)

Sixth field variable.
Etc., up to eight field variables per line.

Repeat this set of data lines as often as necessary to define Y and $α$ as functions of temperature and other predefined field variables.

Data lines to define spatially varying shell section stiffness with a distribution if the MATERIAL, the COMPOSITE, and the USER parameters are omitted

First line

Distribution name. The data in the distribution define the symmetric half of the $[D]$ matrix.

Second line (optional)

${F}$ vector ( $F_{1}$ , $F_{2}$ , ..., $F_{6}$ ).

Third line (optional)

Y, scaling modulus for $[D]$ . The default is 1.0.
$α$ , scaling modulus for $[F]$ . The default is 0.0.
$θ$ , temperature for these values of Y and $α$ .
First field variable.
Second field variable.
Etc., up to five field variables.

Subsequent lines (only needed if the DEPENDENCIES parameter has a value greater than five)

Sixth field variable.
Etc., up to eight field variables per line.

Repeat this set of data lines as often as necessary to define Y and $α$ as functions of temperature and other predefined field variables.

Data lines if the USER parameter is included

First line

Shell thickness. This value is ignored if the NODAL THICKNESS or SHELL THICKNESS parameters are included.

Second line

Enter the data to be used as properties in user subroutine UGENS or VUGENS. Enter all floating point values first, followed immediately by the integer values.

Repeat this data line as often as necessary to define the properties required in user subroutine UGENS or VUGENS. Enter eight values per line for both real and integer values.