BasicQuad#
This command is used to construct a BasicQuad element object which uses the standard Lagrange isoparametric formulation.
- model.element("Quad", tag, nodes, section[, pressure, rho, b1, b2])
- Parameters:
tag – integer, unique element object tag
nodes – tuple, a tuple of four element nodes in counter-clockwise order
section –
tuple or int. If int, it is the tag of a previously defined PlaneSection. If tuple, it is a tuple of the form (
thick
,type
,material
) wherethick
floatelement thickness
type
|str|string representing material behavior. The type parameter can be either
'PlaneStrain'
or'PlaneStress'
material
integertag of an General Materials
pressure – float, surface pressure (optional, default = 0.0)
rho – float, element mass density (per unit volume) from which a lumped element mass matrix is computed (optional, default=0.0)
b1 – float, constant body forces defined in the domain (optional, default=0.0)
b2 – float, constant body forces defined in the domain (optional, default=0.0)
- element quad $eleTag $iNode $jNode $kNode $lNode $thick $type $matTag <$pressure $rho $b1 $b2>
Argument |
Type |
Description |
---|---|---|
$eleTag |
integer |
unique element object tag |
$iNode $jNode $kNode $lNode |
integer four nodes defining element boundaries |
input in counter-clockwise order around the element. |
$thick |
float |
element thickness |
$type |
string |
string representing material behavior. The type parameter can be either “PlaneStrain” or “PlaneStress.” |
$matTag |
integer |
tag of nDMaterial |
$pressure |
float |
surface pressure (optional: default = 0.0) |
$rho |
float |
element mass density (per unit volume) from which a lumped element mass matrix is computed (optional: default=0.0) |
$b1 $b2 |
float |
constant body forces defined in the isoparametric domain (optional: default=0.0) |
The valid eleResponse queries to this element are 'forces'
, 'stresses'
, and 'material $matNum matArg1 matArg2 ...'
where $matNum
refers to the material object at the integration point corresponding to the node numbers in the isoparametric domain.
Consistent nodal loads are computed from the pressure and body forces.
Fig. 27 Quad element node numbering#
Example#
The following example constructs a quad element for use in a plane stress problem with tag 1 between nodes 1, 2, 3, 4 with an nDMaterial of tag 1.
Tcl Code
element quad 1 1 2 3 4 "PlaneStress" 1
Python Code
model.element("quad",1, (1,2,3,4), (1.0, "PlaneStress", 1), (b1, b2, b3))
Code Developed by: Michael H. Scott