Bulk Data Entry Defines the stacking information and stacking sequence
for ply-based composite definition.
Format
(1)
(2)
(3)
(4)
(5)
(6)
(7)
(8)
(9)
(10)
STACK
ID
LAM
PLYID1
PLYID2
PLYID3
PLYID4
PLYID5
PLYID6
PLYID7
etc.
Optional continuation lines for substack definitions:
(1)
(2)
(3)
(4)
(5)
(6)
(7)
(8)
(9)
(10)
SUB
SID1
SNAME1
SPLYID11
SPLYID12
SPLYID13
SPLYID14
SPLYID15
SPLYID16
SPLYID17
etc.
etc.
etc.
etc.
etc.
etc.
etc.
Optional continuation lines for interface definitions:
(1)
(2)
(3)
(4)
(5)
(6)
(7)
(8)
(9)
(10)
INT
IPLYID11
IPLYID12
Optional continuation lines for repeat laminate definitions:
(1)
(2)
(3)
(4)
(5)
(6)
(7)
(8)
(9)
(10)
NRPT
NUMBER
Example 1
Defines a stack consisting of 8 plies with the SMEAR option
(1)
(2)
(3)
(4)
(5)
(6)
(7)
(8)
(9)
(10)
STACK
1
SMEAR
1010100
1020100
1010200
1020200
1010300
1020300
1010400
1020400
Example 2
Defines a stack with substack and interface information. Figure 1. Play Layout
(1)
(2)
(3)
(4)
(5)
(6)
(7)
(8)
(9)
(10)
STACK
2
SUB
1
top
11
12
13
14
SUB
2
left
21
22
23
24
SUB
3
right
31
32
33
34
SUB
4
middle
41
42
43
INT
14
21
INT
14
31
INT
21
41
INT
43
31
Definitions
Field
Contents
SI Unit Example
ID
Unique stack
identification number.
No default (Integer > 0)
LAM
Laminate option. The
following options are supported:
blank (Default)
All plies must be specified and all stiffness terms are
developed.
SYM
Only plies on the bottom half of the composite lay-up
need to be specified. These plies are automatically
symmetrically reflected to the top half of the composite
and given consecutive numbers from bottom to top.
MEM
All plies must be specified, but only membrane terms are
developed.
BEND
All plies must be specified, but only bending terms are
developed.
SMEAR
All plies must be specified, stacking sequence is
ignored, and MID1 is set equal to
MID2 on the derived equivalent
PSHELL,
while MID3, MID4,
TS/T, and
12I/T**3 are set to
blank.
SMEARZ0
All plies must be specified, stacking sequence is
ignored. While the laminate is still considered to be
made of homogenized (smeared) material, the effect of
offset Z0 is taken into account. Hence, if Z0 ≠ -0.5 *
Thick, the equivalent PSHELL will
include MID1, MID2
and MID4. MID3 is
still set to blank, that is no
transverse shear deformation is considered.
SMCORE
All plies must be specified. The last ply specifies core
properties and the previous plies specify face sheet
properties. The face sheet properties are calculated
without regard for stacking sequence; half of the total
face sheet thickness is then placed on top of the core,
and half is placed on the bottom, to produce a symmetric
laminate. Stiffness of the core is ignored while its
density is included in inertia calculations.
SYMEM
Only plies on the bottom half of the composite lay-up
need to be specified. These plies are automatically
symmetrically reflected to the top half of the composite
and given consecutive numbers from bottom to top. Only
membrane terms are developed for the full laminate.
SYBEND
Only plies on the bottom half of the composite lay-up
need to be specified. These plies are automatically
symmetrically reflected to the top half of the composite
and given consecutive numbers from bottom to top. Only
bending terms are developed for the full laminate.
SYSMEAR
Only plies on the bottom half of the composite lay-up
need to be specified. These plies are automatically
symmetrically reflected to the top half of the composite
and given consecutive numbers from bottom to top.
Stacking sequence is ignored, and
MID1 is set equal to
MID2 on the derived equivalent
PSHELL, while
MID3, MID4,
TS/T and
12I/T**3 are set to blank.
PLYID#
PLY identification.
Integer
Specifies an identification number for the ply.
<String>
Specifies a user-defined string label for the ply. 6
The STACK card is used
in combination with the PCOMPP and PLY cards to create composite properties through
the ply-based definition.
Plies are listed from the bottom surface
upward, in respect to the element's normal direction, shown in Figure 2. Figure 2. (A) Stacking Sequence for a Non-symmetrical Laminate; (B) Stacking
Sequence for a Symmetrical Laminate
For convenience, element output for the
SMEAR and SMCORE options includes both
homogenized shell stresses and individual ply stresses. However, because stacking
sequence is ignored in these options, individual ply stresses will only be valid in
cases of pure membrane deformation.
Multiple instances of substack and
interface continuations are allowed.
The repeat laminates are added to the
bottom of the current laminate. Output for repeat laminates are supported in OPTI,
H3D, and PUNCH formats.
String based labels allow for easier
visual identification of ply entries, including when being referenced in the
PLYID# field of STACK entries. For
more details, refer to String Label Based Input File in the
Bulk Data Input File.
This card is represented as a laminate in
HyperMesh.