4.15
TORUS NO.15 WITH 6 NODES
This is a curvilinear
Serendipity torus element with square shape functions. The
transformation is
isoparametric. The integration is carried out numerically according to
Gauss-
Legendre. Thus, the integration order can be selected in Z88I1.TXT in the material information lines. The
order 7 is mostly sufficient. This element calculates both
displacements and
stresses very exactly. The integration order can be chosen again for
the stress
calculation. The stresses are calculated in the corner nodes (good for
an
overview) or calculated in the Gauss points (substantially more
exactly). Pay
attention to edge loads when using forces, cf. chapter 3.4. It is easier to enter edge loads
via the surface and pressure loads file Z88I5.TXT.
This element type is implemented
for use with automeshers e.g. Pro/MECHANICA for
the 3D CAD system Pro/ENGINEER by Parametric Technology. Thus, a mesh
generation with Z88N is not possible. Use torus elements No.8 for Z88N.
Use torus element
No.8
whenever possible. It is substantially more precise than this
isoparametric
triangle.
Input:
CAD (see chapter 2.7.2): 1-4-2-5-3-6-1
Z88I1.TXT
> In principle cylindrical coordinates
are expected: KFLAG must be 0 !
R coordinate (= X), always positive
Z coordinate (= Y), always positive
> IQFLAG=1 if edge loads for this element are filed in Z88I5.TXT
> 2 degrees of freedom for each node, DOF R and Z (= X and Y).
> Element type is 15
> 6 nodes per element
> Cross-section parameter QPARA is 0 or any value, no influence
> Integration order INTORD per each mat info line. 7 is usually
good.
Possible is: 3 for 3 Gauss points, 7 for 7 Gauss points and 13 for 13
Gausspoints. For easy use with torus element No.8 (e.g. with
Pro/ENGINEER),
function ISOD88 of Z88 uses internally these values:
integration order 1 or 2 in Z88I1.TXT: 3 Gauss points
integration order 4 in Z88I1.TXT: 7 Gauss points
Example: Z88I1.TXT uses an entry of 2 for INTORD: Thus, torus
elements No.8
use 2*2 = 4 Gauss points and torus elements No.14 use 3 Gauss points
for
integration.
Z88I3.TXT
> Integration order INTORD: Basically, it is a good idea to
use the
same value as chosen in Z88I1.TXT , but different values are permitted
0 = Calculation of the stresses in the corner nodes
1, 7, 13 = Calculation of the stresses in the Gauss points (e.g. 7
Gauss
points) See note for Z88I1.TXT.
> KFLAG , any, has no influence
> Reduced stress flag
ISFLAG:
0 = no calculation of reduced
stresses
1 = von Mises stresses in the Gauss points ( INTORD not 0 !)
2 = principal stresses in the Gauss points (INTORD not 0!)
3 = Tresca stresses in the Gauss
points (INTORD not 0!)
This file is
optional and only used if in
addition to nodal forces edge loads applied onto element no.15:
>
Element number with surface and pressure
load
>
Pressure, positive if poiting towards the
edge
>
Tangential shear, positive in local r
direction
> 2
corner nodes and one mid node of the
loaded surface
The local r
direction is defined by the nodes
1-2. The local nodes 1, 2, 3 may differ from the local nodes 1, 2, 3
used for
the coincidence.
Results:
Displacements in R and Z (= X and Y).
Stresses: The stresses are calculated in the corner nodes or
Gauss
points and printed along with their locations. It is: SIGRR = stress in
R
direction = radial stress (= X direction), SIGZZ = stress in Z
direction (= Y
direction), TAURZ = shear stress in RZ plane (= XY plane), SIGTE =
stress in
peripherical direction = tangential stress. Optional von Mises stresses.
Nodal forces in R (= X) and Z (= Y) for each element and each
node.