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Code_Aster
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Version
8.2
Titrate:
Operator
POST_ELEM
Date:
22/02/06
Author (S):
X. DESROCHES, L. VIVAN
Key
:
U4.81.22-G1
Page:
1/34
Instruction manual
U4.8- booklet: Postprocessing and dedicated analyzes
HT-62/06/004/A
Organization (S):
EDF-R & D/AMA, CS IF















Instruction manual
U4.8- booklet: Postprocessing and dedicated analyzes
Document: U4.81.22



Operator
POST_ELEM






1 Goal
To calculate quantities on whole or part of the structure. The calculated quantities correspond to
particular options of calculation of affected modeling.
The currently available options are:
·
calculation of the mass, inertias and the position of the center of gravity,
·
calculation of the potential energy,
·
calculation of the kinetic energy,
·
calculation of the work of the external efforts,
·
calculation of the indicators of loss of proportionality of the loading in elastoplasticity,
·
calculation of the limiting load,
·
calculation of the stress of Weibull,
·
calculation of the growth rate of a spherical cavity (Rice - Tracey),
·
calculation of elastic energy and total energy,
·
calculation of the surface of a hole in a mesh 2D.
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Code_Aster
®
Version
8.2
Titrate:
Operator
POST_ELEM
Date:
22/02/06
Author (S):
X. DESROCHES, L. VIVAN
Key
:
U4.81.22-G1
Page:
2/34
Instruction manual
U4.8- booklet: Postprocessing and dedicated analyzes
HT-62/06/004/A
2 Syntax
[tabl_ *] = POST_ELEM
(
# key word simple
MODEL
= Mo,
[model]
CHAM_MATER
=
chmater,
[cham_mater]
CARA_ELEM
=
carac,
[cara_elem]
CHARGE
=
lcha,
/
[l_char_meca]
/
[l_char_ther]
/
[l_char_acou]
|
NUME_COUCHE
=
/
nume,
[I]
/
L,
[DEFECT]
|
NIVE_COUCHE
=
/
“INF”,
/
“SUP”,
/
“MOY”,
[DEFECT]
MODE_FOURIER
=/nh,
[I]
/
0,
[DEFECT]
GEOMETRY =
/“DEFORMATION”,
/
“INITIAL”,
[DEFECT]
/
CHAM_GD
=
cham,
/
[cham_no_DEPL_R]
/
[cham_no_TEMP_R]
/
[cham_elem_ENER_R]
/
RESULT
= resu,
/
[evol_elas]
/
[evol_noli]
/
[evol_ther]
/
[mult_elas]
/
[fourier_elas]
/
[mode_meca]
/
[dyna_trans]
/
TOUT_ORDRE = “YES”,
/
NUME_ORDRE =
l_nuor
,
[l_I]
/
LIST_ORDRE =
l_ordr
,
[listis]
/
NUME_MODE
=
l_numo
,
[l_I]
/
NOEUD_CMP
=
l_nomo
,
[l_Kn]
/
NOM_CAS =
l_nocas,
[l_Kn]
/
/
FREQ =
l_freq
,
[l_R]
/LIST_FREQ
=
lreel
,
[listr8]
/
/
INST =
l_inst
,
[l_R]
/LIST_INST
=
lreel
,
[listr8]
|
PRECISION =/prec, [R]
/
1.0D-3
,
[DEFECT]
|
CRITERION
=/“RELATIVE”, [DEFECT]
/
“ABSOLUTE”
,
# key words factor
|
MASS_INER: (see key word MASS_INER
[§ 3.9])
|
ENER_POT: (see key word ENER_POT
[§ 3.10])
|
ENER_CIN: (see key word ENER_CIN
[§ 3.11])
|
ENER_ELAS: (see key word ENER_ELAS
[§ 3.12])
|
ENER_TOTALE: (see key word ENER_TOTALE
[§ 3.13])
|
WEIBULL: (see key word WEIBULL
[§ 3.14])
|
RICE_TRACEY: (see key word RICE_TRACEY [§ 3.15])
|
INDIC_ENER: (see key word INDIC_ENER [§ 3.16])
|
INDIC_ THRESHOLD: (see key word INDIC_ THRESHOLD [§ 3.17])
|
CHAR_LIMITE: (see key word CHAR_LIMITE
[§ 3.18])
|
CARA_GEOM: (see key word CARA_GEOM
[§ 3.19])
|
CARA_POUTRE: (see key word CARA_POUTRE [§ 3.20])
|
AIRE_INTERN: (see key word AIRE_INTERN [§ 3.21])
|
TRAV_EXT
: (see key word TRAV_EXT
3.22]
)
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Code_Aster
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Version
8.2
Titrate:
Operator
POST_ELEM
Date:
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Author (S):
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Key
:
U4.81.22-G1
Page:
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HT-62/06/004/A

INFORMATION
=
/
1,
[DEFECT]
/2,
TITRATE = Ti,
)

The table result of the operator
POST_ELEM
is a typified table
if
MASS_INER
then * =
mass_iner
if
ENER_POT
then * =
ener_pot
if
ENER_CIN
then * =
ener_cin
if ENER_ELAS
then * =
ener_elas
if ENER_TOTALE
then * =
ener_totale
if
WEIBULL
then * =
weibull
if
RICE-TRACEY
then * =
rice_tracey
if
INDIC_ENER
then * =
indic_ener
if
INDIC_SEUIL
then * =
indic_seuil
if
CHAR_LIMITE
then * =
char_limite
if
CARA_GEOM
then * =
cara_geom
if
CARA_POUTRE
then * =
cara_geom
if AIRE_INTERN
then * =
aire_int
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Code_Aster
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Version
8.2
Titrate:
Operator
POST_ELEM
Date:
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Author (S):
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Key
:
U4.81.22-G1
Page:
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3 Operands
3.1 Operand
MODEL
MODEL = Mo,
Name of the model on which the option is calculated. The name of the model is optimal because it is contained
in the structure of data result.

3.2 Operand
CHAM_MATER
CHAM_MATER = chmater,
Material field associated with the model
Mo
, optimal bus contained in the structure of data
result.

3.3 Operand
CARA_ELEM
CARA_ELEM = carac,
Elementary characteristics
carac
are necessary if there exists in the model of the elements
of structure (discrete beam, plate, hull or elements), optimal bus contained in the structure of
data result.

3.4 Operand
CHARGE
CHARGE = lcha,
List containing the concepts of the type
charge
, optimal bus contained in the structure of data
result.

3.5 Operands
NUME_COUCHE/NIVE_COUCHE
NUME_COUCHE = nume,
In the case of a multi-layer material, whole value ranging between 1 and number it layers,
necessary to specify the layer where one wishes to carry out elementary calculation. By convention,
layer 1 is the sub-base in the case of the elements of mechanical hull or hull
thermics.
NIVE_COUCHE =
For the layer
nume
defined by
NUME_COUCHE
, allows to specify the ordinate where one wishes
to carry out elementary calculation:
“INF”
lower ordinate of the layer
(skin interns),
“SUP”
higher ordinate of the layer
(external skin),
“MOY”
average ordinate of the layer
(average layer by defect).
3.6 Operand
MODE_FOURIER
MODE_FOURIER =
Number of the harmonic of FOURIER: positive or null entirety (defect = 0).
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Code_Aster
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Titrate:
Operator
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Date:
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U4.81.22-G1
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3.7 Operand
GEOMETRY
GEOMETRY =
/“INITIAL”,
[DEFECT]
/“DEFORMATION”,
Indicate if one works on the initial geometry or the deformation. In this last case, it is necessary
to provide a field of displacements by CHAM_GD or RESULT.
3.8 Operands
CHAM_GD
/
RESULT
Options
ENER_POT
and
ENER_CIN
are calculated starting from a field with the nodes or by elements
existing or extracted from one
result
.
3.8.1 Operand
CHAM_GD
/CHAM_GD = cham,
Name of a field (for options ENER_POT and ENER_CIN).
For the option
ENER_POT
, it is necessary to provide a field of displacement or a field of
temperature (see [§3.9]).
For the option
ENER_CIN
, it is necessary to provide a field speed (without providing frequency) or
well a field of displacements and a frequency (see [§3.9]).
3.8.2 Operand
RESULT
/RESULT = resu,
Name of a concept result of the type
evol_elas
,
evol_ther
,
mode_meca
,
evol_noli
,
mult_elas
,
fourier_elas
or
dyna_trans
.
Option ENER_POT:
evol_elas
,
evol_ther
,
mode_meca
,
mult_elas
,
Fourier elas
evol_noli
, or
dyna_trans
.
Option ENER_CIN:
mode_meca
,
evol_elas,
evol_ther,
evol_noli, or
dyna_trans
.
Option ENER_ELAS and ENER_TOTALE: evol_noli.

3.8.2.1 Operands TOUT_ORDRE/NUME_ORDRE/NUME_MODE/LIST_ORDRE/NOEUD_CMP/FREQ/
LIST_FREQ/INST/LIST_INST/PRECISION/CRITERION
See [U4.71.00].
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Code_Aster
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Titrate:
Operator
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Date:
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Key
:
U4.81.22-G1
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3.9 Word
key
MASS_INER
3.9.1 Drank
Key word factor allowing to calculate the mass, inertias and the center of gravity.
This option allows calculation on each element of the following characteristics:
(
indicating the density defined in
DEFI_MATERIAU
[U4.43.01] by
ELAS
or
ELAS_FO
).
()
(
) (
)
(
)
()
(
) (
)
()
(
) (
)
(
)
()
(
) (
)
()
(
) (
)
(
)
()
(
) (
)
FD
Z
Z
y
y
G
I
FD
y
y
X
X
G
I
FD
Z
Z
X
X
G
I
FD
Z
Z
X
X
G
I
FD
y
y
X
X
G
I
FD
Z
Z
y
y
G
I
FD
Z
v
Z
FD
y
v
y
FD
X
v
X
FD
m
v
G
G
yz
v
G
G
zz
v
G
G
xz
v
G
G
yy
v
G
G
xy
v
G
G
xx
v
G
v
G
v
G
v
-
-
=
-
+
-
=
-
-
=
-
+
-
=
-
-
=
-
+
-
=
=
=
=
=
2
2
2
2
2
2
:
1
;
1
;
1
:
:
mesh
N
descriptio
of
global'
'
identify
in
G
gravity
of
center
with
inertia
of
Tensor
gravity
of
Center
Mass
Then calculates by “summation” the quantities relating to the total structure.
3.9.2 Syntax
|
MASS_INER
=_F
(
TAILLE_BLOC=
/400
,
[DEFECT]
/
tbloc,
[R]
/ALL = “YES”,
/
NET
=
l_maille,
[l_maille]
/
GROUP_MA=
lgrma,
[l_gr_maille]
ORIG_INER= (xp, YP [, zp]), [l_R]
),
Simple key words: (see [§2])
MODEL
= Mo,
[model]
CHAM_MATER
=
chmater,
[cham_mater]
CARA_ELEM
=
carac,
[cara_elem]
|
NUME_COUCHE
=
|
NIVE_COUCHE
=
MODE_FOURIER
=
GEOMETRY =
/CHAM_GD
=
/
RESULT
=
CHARGE
=
/
[char_meca]
/[char_ther]
/[char_acou]
Note
For the key word factor
MASS_INER
, the material model and field are
obligatory.
If one wants to calculate the quantities on a deformed geometry, one will use the key word
GEOMETRY and one will re-enter a field of displacements by CHAM_GD or RESULT.
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3.9.3 Operands
/ALL = “YES”,
On all the structure.
/
NET = l_maille,
On a list of meshs.
/
GROUP_MA
= lgrma,
On a list of group of meshs.
ORIG_INER = (xp, YP [, zp]),
[l_R]
Not by report/ratio to which the tensor of inertia will be calculated.
The tensor of inertia at the point
P
co-ordinates (xp, YP, zp) is obtained starting from the tensor
of inertia in the center of gravity
G
, of the mass
m
structure and co-ordinates of
G
by
formulas:
()
()
()
()
()
()
()
()
()
()
()
()
I
P
I
G
m X
I
P
I
G
m y
I
P
I
G
m Z
I
P
I
G
m X
y
I
P
I
G
m X
Z
I
P
I
G
m y
Z
X
X
X
y
y
y
Z
Z
Z
xx
xx
PG
yy
yy
PG
zz
zz
PG
xy
xy
PG PG
xz
xz
PG PG
yz
yz
PG PG
PG
G
P
PG
G
P
PG
G
P
=
+
=
+
=
+
=
+
=
+
=
+
=
-
=
-
=
-
2
2
2
with
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Titrate:
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3.10 Word
key
ENER_POT
3.10.1 Drank
Key word factor allowing to calculate:
·
potential energy of deformation due to balance starting from displacements, in
linear mechanics of the continuous mediums (2D and 3D):
() ()
()
()
()
()
+
-
=
element
HT
HT
element
HT
element
FD
T
With
T
FD
T
With
FD
With
EPOT
.
2
1
.
.
2
1
U
U
U
where
With
indicate the tensor of elasticity,
·
potential energy of deformation due to balance starting from displacements, in
linear mechanics for the elements of structures:
HT
HT
HT
T
E
T
EPOT
With
With
B
U
U
K
U
T
2
1
2
1
+
-
=
where
K
indicate the matrix of rigidity
·
the energy dissipated thermically with balance in linear thermics from
temperatures (
cham_no_TEMP_R
):
W
HT
T
T D
= +
1
2
. K.
.
Note:
In the first both cases, one must give a field of displacement behind
the operand
RESULT
or
CHAM_GD
. In the last case a field of temperature.
In any rigor, the potential energy of a structure is negative. Here one calculates
rather a deformation energy.
3.10.2 Syntax
|
ENER_POT
=_F
(
/ALL = “YES”,
/
NET
=
l_maille,
[l_maille]
/
GROUP_MA=
lgrma,
[l_gr_maille]
)
Simple key words: (see [§2])
MODEL
= Mo,
[model]
CHAM_MATER
=
chmater,
[cham_mater]
CARA_ELEM
=
carac,
[cara_elem]
|
NUME_COUCHE
=
|
NIVE_COUCHE
=
MODE_FOURIER
=
/CHAM_GD
=
/
RESULT
=
CHARGE
=
CH,
/
[char_meca]
/[char_ther]
/[char_acou]
Note
For the key word factor
ENER_POT
, the model, the field of materials and possibly it
field of characteristics of elements of structure are obligatory to determine with
precondition fields of energy by elements.
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Titrate:
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3.10.3 Operands
/ALL = “YES”,
On all the structure.
/
NET = l_maille,
On a list of meshs.
/
GROUP_MA
= lgrma,
On a list of group of meshs.
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Operator
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Date:
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:
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3.11 Word
key
ENER_CIN
3.11.1 Drank
Key word factor allowing to calculate the kinetic energy starting from a field speed or to leave
of a field of displacement and a frequency.
If a field speed were given,
E
V MV
C
T
= 12
.
If one gave a field of displacement and a frequency,
E
U DRIVEN
C
T
= 12
2
.
3.11.2 Syntax
|
ENER_CIN
=_F
(
/ALL = “YES”,
/
NET
=
l_maille,
[l_maille]
/
GROUP_MA=
lgrma,
[l_gr_maille]
)
Simple key words: (see [§2])
MODEL
= Mo,
[model]
CHAM_MATER
=
chmater,
[cham_mater]
CARA_ELEM
=
carac,
[cara_elem]
|
NUME_COUCHE
=
|
NIVE_COUCHE
=
MODE_FOURIER =
OPTION =/“MASS_MECA”,
/“MASS_MECA_DIAG”,
/CHAM_GD
=
/
RESULT
=
CHARGE
=
CH,
/
[char_meca]
/[char_ther]
/[char_acou]
Note 1
For the key word factor
ENER_CIN
, the model, the field of materials and possibly it
field of characteristics of elements of structure are obligatory to determine with
precondition fields of energy by elements.
Note 2
When one wishes to calculate energy by employing the diagonal mass (to be in
coherence with the option which one chose in the elementary calculation of the matrices of
mass), one can specify “MASS_MECA_DIAG” behind the key word OPTION (nonavailable
in 2D). By defect one uses the matrix of complete mass.
3.11.3 Operands
/ALL = “YES”,
On all the structure.
/
NET = l_maille,
On a list of meshs.
/
GROUP_MA
= lgrma,
On a list of group of meshs.
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3.12 Word
key
ENER_ELAS
3.12.1 Drank
Allows to calculate the elastic deformation energy for each moment
T
after an elastic design
or elastoplastic, starting from the stress field SIEF_ELGA or SIEF_ELGA_DEPL by
the expression:
()
()
()
E T
T D
T FD
E
T
v
=
-
1
2
1
where
D
represent the operator of elasticity.
3.12.2 Syntax
|
ENER_ELAS
=_F
(
/ALL = “YES”,
/
NET
=
l_maille,
[l_maille]
/
GROUP_MA=
lgrma,
[l_gr_maille]
)
Simple key words: (see [§2])
MODEL
= Mo,
[model]
CHAM_MATER
=
chmater,
[cham_mater]
CARA_ELEM
=
carac,
[cara_elem]
|
NUME_COUCHE
=
|
NIVE_COUCHE
=
MODE_FOURIER
=
RESULT =
CHARGE
=
/
[char_meca]
/[char_ther]
/[char_acou]
3.12.3 Operands
/ALL = “YES”,
On all the structure.
/
NET = l_maille,
On a list of meshs.
/
GROUP_MA = lgrma,
On a list of group of meshs.
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3.13 Word
key
ENER_TOTALE
3.13.1 Drank
Key word factor allowing to calculate the total deformation energy for the elements of mediums
continuous 2D or 3D with behavior VMIS_ISOT_LINE or VMIS_ISOT_TRAC (work hardening
isotropic), starting from the material and internal variable, stress fields:
()
E
E
E
With
FD
R Q dq FD
T
el
P
T
P
v
v
=
+
=
+



-
1
2
1
0
P
being cumulated equivalent plastic deformation.
With the option
SIMO_MIEHE
, this energy applies to the two models
VMIS_ISOT_LINE
or
VMIS_ISOT_TRAC
:
E
D FD
T
T
v
=
+






0
0
0
where
and
are respectively the free energy and the potential of dissipation,
V
0
initial volume.
For more precision, to see [R5.03.21].
3.13.2 Syntax
|
ENER_TOTALE = _F (
/ALL = “YES”,
/
NET
=
l_maille,
[l_maille]
/
GROUP_MA=
lgrma,
[l_gr_maille]
)
Simple key words: (see [§2)
MODEL
= Mo,
[model]
CHAM_MATER
=
chmater,
[cham_mater]
CARA_ELEM
=
carac,
[cara_elem]
|
NUME_COUCHE
=
|
NIVE_COUCHE
=
MODE_FOURIER
=
RESULT
=
CHARGE
=
CH,
/
[char_meca]
/[char_ther]
/[char_acou]
3.13.3 Operands
/ALL = “YES”,
On all the structure.
/
NET = l_maille,
On a list of meshs.
/
GROUP_MA = lgrma,
On a list of group of meshs.
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3.14 Word
key
WEIBULL
3.14.1 Drank
Key word allowing for each defined moment, the calculation of the elementary field of the power
m ième
-
stress of Weibull of which the expression on the mesh
K
is given, without catch in
count plastic deformation, by:
()
wm
ref.
m
K
p
K
V
dK
p
=
1
1
and, with taking into account of the plastic deformation by:
()
wm
ref.
m
K
p
p
K
V
Exp
m
dK
p
=
-




1
2
1
1
K
p
indicate the part of the mesh
K
who plasticized, i.e., the part of
K
where deformation
figure cumulated exceeds a certain threshold;
1
represent the maximum main stress and
1p
represent the maximum main plastic deformation.
The parameters material
m V
ref.
,
and the threshold of plasticity are defined in DEFI_MATERIAU by
relation of behavior WEIBULL (cf [R7.02.06]).
Once determined this elementary field, the option calculates by “summation” the stress of Weibull
of a field
D
for each definite moment:
()
()
W
wm
K D
m
D
C
K
=


1
where
C
is a coefficient intended for the taking into account of symmetries (case Bi and three-dimensional) and of
the thickness (in the two-dimensional case) of the structure containing the field
D
(key word
COEF_MULT).
The probability of rupture of the field D is then calculated by:
()
P D
Exp
W
wm
um
= -
-






1

.
The parameter “forced of cleavage”
µ
is, him also, defined in the relation of behavior
WEIBULL.
Lastly, the preceding expressions of the stress of Weibull and the probability of rupture are not
valid that in the case of a monotonous way of loading. This type of postprocessing can
nevertheless also to be applied to a way of more general loading, including when the stress
on cleavage depends on the temperature (relation of behavior WEIBULL_FO). Expressions of
forced of Weibull and the probability of rupture are then different (cf [R7.02.06]).
Note:
For the key word factor WEIBULL, the model and the field of material are obligatory.
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3.14.2 Syntax
|
WEIBULL = _F (
/
ALL =
“YES”,
/
NET
=
l_maille
,
[l_maille]
/
GROUP_MA = lgrma,
[l_gr_maille]
OPTION
=
/
“SIGM_ELGA”,
[DEFECT]
/
“SIGM_ELMOY”,
CORR_PLAST=
/
“YES”,
/
“NOT”,
[DEFECT]
COEF_MULT
=
/
coeff,
[R]
/
1., [DEFECT]
)
Simple key words: (see [§2])
MODEL
= Mo,
[model]
CHAM_MATER
=
chmater,
[cham_mater]
CARA_ELEM
=
carac,
[cara_elem]
|
NUME_COUCHE
=
|
NIVE_COUCHE
=
MODE_FOURIER
=
/CHAM_GD
=
/
RESULT
=
CHARGE
=
/
[char_meca]
/[char_ther]
/[char_acou]
3.14.3 Operands
3.14.3.1 Operand
OPTION
/OPTION = “SIGM_ELGA”,
The value of the elementary field associated the mesh
K
is obtained by integration by
quadrature at the points of Gauss of the expression
1
1
V
dK
p
m
K
p
.
/
OPTION = “SIGM_ELMOY”,
The value of the elementary field associated the mesh
K
is obtained starting from the value
main maximum of the tensor
1
V
dK
p K
p
whose value is approached by
quadrature at the points of Gauss.

3.14.3.2 Operand
CORR_PLAST
/CORR_PLAST = “YES”,
The stress field of Weibull is evaluated with taking into account of the deformation
plastic.
/
CORR_PLAST
=
“NOT”,
The stress field of Weibull is evaluated without taking into account of the deformation
plastic.
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3.14.3.3 Operand COEF_MULT
/COEF_MULT = value,
The default value of this coefficient is 1.0D0.
The following table, in which the thickness is noted
E
, indicates typical values of
coefficient
C
according to the type of symmetry:
·
simple symmetry: the symmetry plane of the mesh passes by the plan of the defect and it
defect is entirely with a grid,
·
double symmetry: the symmetry plane of the mesh also passes by the plan of
defect but only one half of the defect is with a grid.
3D and 3d_SI
AXIS and
AXIS_SI
D_PLAN and
D_PLAN_SI
C_PLAN
SIMPLE
2
4
2
E
2
E
DOUBLE
4
without object
without object
without object
NOT
1
2
E
E
Values of the multiplying coefficient symmetry-thickness
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3.15 Word
key
RICE_TRACEY
3.15.1 Drank
This option allows, for each moment of calculation
T
N
defined, the calculation of the growth rate
()
R T
R
N
-
0
of a spherical cavity compared to a field
()
(
D R T
N
and
R
0
indicate the radius respectively
running and the initial radius of the cavity). The law of evolution of Rice-Tracey is expressed by the relation:
D
dt Log
R
R
Sign
Exp
D
dt
M
eq
M
eq
eq
p
0
0 283
3
2




=






,
(
()
M
Trace
= 13
;
eq
indicate the equivalent stress of von Mises and
eq
p
indicate
equivalent deformation of von Mises).

3.15.2 Syntax
|
RICE_TRACEY = _F (
/
ALL =
“YES”,
/
NET
=
l_maille, [l_maille]
/
GROUP_MA = lgrma,
[l_gr_maille]
OPTION
=
/
“SIGM_ELGA”,
[DEFECT]
/
“SIGM_ELMOY”,
ROOM
=
/
“YES”,
[DEFECT]
/
“NOT”,
)
Simple key words: (see [§2])
MODEL
= Mo,
[model]
CHAM_MATER
=
chmater,
[cham_mater]
CARA_ELEM
=
carac,
[cara_elem]
|
NUME_COUCHE
=
|
NIVE_COUCHE
=
MODE_FOURIER
=
/CHAM_GD
=
/RESULT
=
CHARGE
=
CH,
/
[char_meca]
/[char_ther]
/[char_acou]
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3.15.3 Operands

3.15.3.1 Operand OPTION
OPTION
=
/
“SIGM_ELGA”,
[DEFECT]
The elementary fields of the stresses and the plastic deformations are used in theirs
representations at the points of Gauss.
/
“SIGM_ELMOY”,
The elementary fields of the stresses and the plastic deformations are realized by
report/ratio at the points of Gauss before being used.

3.15.3.2 Operand ROOM
ROOM
=
/
“YES”,
[DEFECT]
The law of Rice-Tracey is integrated on each mesh
K
field
D
and the result consists
in the maximum value obtained on the whole of the meshs of the field.
/
“NOT”,
Fields of triaxiality
()
M
eq
N
T
and of variation of plastic deformation
()
eq
p
N
T
are
calculated on each mesh. Then, their respective averages, balanced by the volume of
meshs of the field, are given. Finally, the law of Rice-Tracey is integrated on these
realized values.

3.15.3.3 Operands ALL/GROUP_MA/MESH
Fields of calculation
D
are specified by:
/ALL = “YES”,
Only one field is defined, it coincides with the whole of the structure.
/GROUP_MA = lgrma,
Each definite group of meshs of the list lgrma a field of calculation.
/MESH = l_maille,
Each mesh of the list l_maille definite a field of calculation.
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3.16 Word
key
INDIC_ENER
3.16.1 Drank
Key word factor allowing to calculate a total indicator of loss of proportionality of the loading
in elastoplasticity, founded on the density of energy. This indicator is described in detail in the document
[R4.20.01].
One points out his function and his expression. This indicator is intended to detect if during
history of the structure and until the current moment T, and for a zone of the structure chosen by
modelisator, there was loss of proportionality of the loading (i.e it acts to have a total measurement
change of the main directions of the tensor of stresses for each point of the area
defined by the user).
This indicator is usable only for models whose material presents a work hardening
isotropic and whose elements are isoparametric 2D or 3D.
This indicator has as an expression:
I
V
FD
v
=
-




1
1
where:
·
V
is the volume of the field defined by the user,
·
is the density of total elastic energy associated the traction diagram if one
considered the non-linear elastic material.
More exactly its expression is as follows:
()
()
()
()
()
()
=
+
<
=
+
+
=
1
2
2 3
1
2
6
2
2
2
2
K tr
R p
K tr
R p
R S ds
R p
eq
eq
O
p
eq
.
.
µ
µ
if
if
where:
·
K
is the module of compressibility,
·
µ
is the coefficient of shearing of Lamé,
·
()
R p
is the threshold of the traction diagram associated with the deformation
figure cumulated
p
,
·
is the density of deformation energy defined by:
()
T
D
O
T
=
.
&
one can break up
()
T
in an elastic part and a plastic part:
()
()
()
T
T
T
élas
plas
=
+
with:
()
()
()
élas
élas
plas
O
T
T
T
R p D p
=
=
1
2
.
Note:
If one has
()
T = 0
, one poses
I
= 0
.
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3.16.2 Syntax
|
INDIC_ENER = _F (
/
ALL =
“YES”,
/
NET
=
l_maille, [l_maille]
/
GROUP_MA = lgrma,
[l_gr_maille]
)
Simple key words: (see [§2])
MODEL
= Mo,
[model]
CHAM_MATER
=
chmater,
[cham_mater]
CHARGE
=
CH,
/
[char_meca]
/[char_ther]
/[char_acou]
RESULT = resu, [evol_noli]

3.16.3 Operands
The indicator is calculated on the field defined by the key words:
/
ALL = “YES”,
On all the elements of the model
Mo
.
/
NET = l_maille,
On the list
l_maille
meshs of the model
Mo
.
/
GROUP_MA = lgrma,
On the list
lgrma
groups of meshs of the model
Mo
.
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3.17 Word
key
INDIC_SEUIL
3.17.1 Drank
Key word factor allowing to calculate a total indicator of loss of proportionality of the loading
in elastoplasticity.
This indicator makes it possible on the one hand to know, on average about the area considered, if the tensor of
stresses and that of the plastic deformations have the same directions and if the plastic threshold is
reached at the current moment, and in addition if during the history the plastic deformation changed
direction.
This indicator has as an expression:
()
I
V
R p p FD
p
v
=
-


1
1
.
.
where:
·
V
is the volume of the field defined by the user,
·
is the tensor of the stresses at the moment running,
·
p
is the tensor of the plastic deformations at the moment running,
·
()
R p
is related to work hardening (with
()
R O
y
=
where
y
is the limit
of elasticity).
i.e. it is the threshold of the traction diagram associated with the cumulated plastic deformation
p
.
·
p
is the cumulated plastic deformation.
Note:
If one has
()
R p p
.
= 0
, one poses
I
= 0
.
The scalar product
.
p
is associated the standard within the meaning of von Mises.
This indicator is standardized and has a value ranging between 0 and 1.
It is null if the loading preserved its character proportional in each point of
V
all with length
past history.
This indicator is described in detail in the document [R4.20.01].
3.17.2 Syntax
|
INDIC_SEUIL = _F (
/
ALL =
“YES”,
/
NET
=
l_maille
,
[l_maille]
/
GROUP_MA = lgrma,
[l_gr_maille]
)
Simple key words: (see [§2])
MODEL
= Mo,
[model]
CHAM_MATER
=
chmater,
[cham_mater]
CHARGE
=
CH,
/
[char_meca]
/[char_ther]
/[char_acou]
RESULT = resu, [evol_noli]
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3.17.3 Operands
The indicator is calculated on the field defined by the key words:
/
ALL = “YES”,
On all the elements of the model
Mo
.
/
NET = l_maille,
On the list
l_maille
meshs of the model
Mo
.
/
GROUP_MA = lgrma,
On the list
lgrma
groups of meshs of the model
Mo
.
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3.18 Word
key
CHAR_LIMITE
3.18.1 Drank
Post_traitement of the calculation of the limiting load [R7.07.01 §2.3].
This key word factor allows the calculation of the limiting load of a structure by a kinematic approach.
Its employment requires as a preliminary to have carried out a nonlinear calculation (see operator
STAT_NON_LINE [U4.51.03]) indicated by the key word RESULT and whose characteristics are them
following:
·
law of behavior NORTON_HOFF,
·
increasing list of moments of calculation corresponding to values of regularization of the law of
NORTON_HOFF which tends towards 1 (in practice, one recommends to be limited to moments
ranging between 1 and 2 which does not lead to too long calculations while allowing
to obtain an upper limit of the load limits sufficiently precise),
·
loading (unit) controlled corresponding to the loading by report/ratio to which one seeks with
to consider the limiting load, the method of piloting being STANDARD = “ANA_LIM”,
·
possibly a constant loading whose it is then necessary imperatively to point out the existence
by key word CHAR_CSTE
= “YES”.
Operator POST_ELEM then produces a table which gives for each moment of calculation, i.e.
for increasingly weak regularizations, a limit upper CHAR_LIMI_SUP of the load
limit supported by the structure. Moreover, in the absence of constant loading, CHAR_CSTE
=
“NOT”, the table also contains an estimate CHAR_LIMI_ESTIM of a lower limit of
charge limit. On the other hand, if a constant loading is present, CHAR_CSTE
= “YES”, such
estimate of the lower limit is not available any more but the table contains the power then
PUIS_CHAR_CSTE of the constant loading in the field speed solution of the problem.
A detailed example of calculation of limiting load is provided in [U2.05.04].

3.18.2 Syntax
|
CHAR_LIMITE = _F (
CHAR_CSTE
=/
'
NOT
'
,
[DEFECT]
/
'
YES
'
,
)
Simple key words: (see [§2])
MODEL
= Mo,
[model]
CHAM_MATER
=
chmater,
[cham_mater]
RESULT
= resu,
[evol_noli]
CARA_ELEM
=
carac,
[cara_elem]
MODE_FOURIER
= nh,
[I]
CHARGE
= CH,
/
[char_meca]
/[char_ther]
/[char_acou]
3.18.3 Operands
CHAR_CSTE
=/
'
NOT
'
,
[DEFECT]
/
'
YES
'
,
Key word indicating if the loading is constant or not constant (default value).
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3.19 Word
key
CARA_GEOM
3.19.1 Drank
CARA_GEOM
is used by the macro_commande
MACR_CARA_POUTRE
[U4.42.02] to calculate them
geometrical characteristics (center of inertia, moments of inertia) of a section of beam with a grid in
elements of continuous medium 2D.
3.19.2 Syntax
|
CARA_GEOM = _F
(
/ALL = “YES”,
/
GROUP_MA=
lgma,
[l_gr_maille]
/
NET
=
lma
,
[l_maille]
SYME_X =/“YES”,
/
“NOT”,
[DEFECT]
SYME_Y =/“YES”,
/
“NOT”,
[DEFECT]
ORIG_INER
=
(xp,
YP),
[l_R]
)
Single-ended spanner words: (see [§2])
MODEL
=
Mo,
[model]
CHAM_MATER
=
chmater,
[cham_mater]
CHARGE
=
CH,
/
[char_meca]
/
[char_ther]
/
[char_acou]
3.19.3 Operands

3.19.3.1 Operands ALL/GROUP_MA/MESH
Define the place of calculation. One can in particular make the calculation of the characteristics for one
together of meshs, defined by GROUP_MA or MESH.

3.19.3.2 Operands
SYME_X
/
SYME_Y
Taking into account of a symmetry compared to X or with Y (or both). Mesh provided by the user
corresponds then to half of the section (or the quarter).

3.19.3.3 Operand
ORIG_INER
Allows to give the punctual coordinates per report/ratio to which the characteristics will be calculated
geometrical [U4.42.02].
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3.20 Word
key
CARA_POUTRE
3.20.1 Drank
CARA_POUTRE
is used exclusively by the macro-control
MACR_CARA_POUTRE
[U4.42.02]
to calculate the mechanical characteristics (constant of torsion, radius of torsion, constants of
shearing, position of the center of shearing, constant of roll) of a section with a grid in
elements 2D.
Its employment requires the preliminary call of many controls, specific to each option
calculated. The operands will thus not be here detailed. For more detail one will refer to
MACR_CARA_POUTRE
[U4.42.02].
3.20.2 Syntax
|
CARA_POUTRE = _F (
/ALL = ' OUI',
/
GROUP_MA
=lgma,
[gr_maille]
GROUP_MA_INTE= lgma_inte,
[l_gr_maille]
CARA_GEOM =
,
[tabl_cara_geom]
LAPL_PHI =
,
[evol_ther]
LAPL_PHI_Y=
y,
[evol_ther]
LAPL_PHI_Z=
Z,
[evol_ther]
RT=
rt,
[R]
CONNECTION
=
/“BALL JOINT”,
/
“EMBEDDING”,
LENGTH
=
L,
[R]
MATERIAL = chechmate
,
[to subdue]
OPTION
=/“CARA_TORSION”,
/
“CARA_CISAILLEMENT”,
/
“CARA_GAUCHI”,
)
Single-ended spanner words: (see [§2])
MODEL
=
Mo,
[model]
CHAM_MATER
=
chmater,
[cham_mater]
CHARGE
=
CH,
/
[char_meca]
/
[char_ther]
/
[char_acou]
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3.21 Word
key
AIRE_INTERN
3.21.1 Drank
Key word factor allowing the calculation of the surface of a hole in a mesh 2D.

3.21.2 Syntax
|
AIRE_INTERN = _F
(
GROUP_MA_BORD = lgma)
Single-ended spanner word:
MODEL
=
Mo,
[model]

3.21.3 Operand
GROUP_MA_BORD = lgma,
List groups of meshs of edge delimiting hole (SEG2 or SEG3)
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3.22 Word
key
TRAV_EXT
3.22.1 Drank
Mot_clé factor allowing to calculate the work of external efforts real TRAV_REEL or rubber band
TRAV_ELAS such as below definite:
=
=
T
T
T
T
0
0
TRAV_REEL
U
F
int
&
&
éq
3.22.1-1
U
F
int
=
=
2
1
2
1
TRAV_ELAS
éq
3.22.1-2
Calculation is carried out on the basis of SD result, well informed under the key word RESULT, for
which nodal forces, i.e. the interior forces, were calculated beforehand by
the operator CALC_ELEM, option “FORC_NODA” [U4.81.01]. In the case of real work, the initial moment
0
T
corresponds to the first moment filed in the SD result (taking guard with the fact that the initial state is not
not filed automatically, to see key word ARCH_ETAT_INIT of operator STAT_NON_LINE
[U4.51.03]); integration in time is carried out by a method of trapezoids. Two sizes
TRAV_REEL and TRAV_ELAS are calculated for each moment filed in the SD result.
These quantities can be interpreted graphically on the response curve forces ­ displacement of
the structure (provided that the force is dual displacement, for example pressure and volume
in the case of a cavity under pressure).

displacement
displacement
force force
TRAV_REEL
TRAV_ELAS
A detailed example of use of these sizes to evaluate the dual size of the loading,
dissipated energy or the residual rigidity of a damaged structure is provided by the study
of a structure which is damaged in a fragile way [U2.05.02].
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8.2
Titrate:
Operator
POST_ELEM
Date:
22/02/06
Author (S):
X. DESROCHES, L. VIVAN
Key
:
U4.81.22-G1
Page:
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3.22.2 Syntax
TRAV_EXT = _F
(
RESULT
=
resu
)
/
[evol_elas]
/
[evol_noli]
/
[dyna_trans]

3.22.3 Operand
RESULT = resu
Name of the structure of data result of calculation.

3.23 Operand
TITRATE
TITRATE
= Ti,
Titrate attached to the concept produced by this operator [U4.03.01].

3.24 Operand
INFORMATION
INFORMATION
=
/
1, [DEFECT]
/2,
Parameter of impression
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Titrate:
Operator
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:
U4.81.22-G1
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4 Example
The example which follows applies to the calculation of total quantities to a dynamic modeling of one
ship jet engine. Are modelized: the external chamber, the interior chamber, internal structures,
the well of tank.


Noncontractual modeling
60 m
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Titrate:
Operator
POST_ELEM
Date:
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Key
:
U4.81.22-G1
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The modeling of a half ship is carried out by elements of beams, discrete elements
representing the connections on the ground, the masses additional and the connections between nodes.
It is on this model of beams that the operator
POST_ELEM
will calculate:
·
mass of the structure,
·
co-ordinates of the center of gravity,
·
the tensor of inertia,
·
potential energy of certain modes and its distribution in the structure,
·
kinetic energy of certain modes and its distribution in the structure.
4.1
Calculation of the mass, the center of gravity and inertias
·
for all the structure (
ALL = “YES”
)
·
for the group of meshs containing the beams (
GROUP_MA = “pou_d_t'
)
·
for the group of meshs containing the connections on the ground (
GROUP_MA = “liai_sol”
)
·
for the group of meshs containing the additional masses (
GROUP_MA = “masses”
)
·
for the group of meshs containing the connections between nodes (
GROUP_MA = “liai_noe”
)
Order
massestr = POST_ELEM (MODELE= stickmod,
CHAM_MATER = chmater, CARA_ELEM = caraelem,
MASS_INER=_F (GROUP_MA= (“pou_d_t', “liai_sol”, “masses”, “liai_noe”),
TOUT=
“YES”,),
TITER=' masses, center of revolves and inertias of the structure');
Impression on the file
“RESULT”
---------------------------------------------------------------------------
mass, center of revolves and inertias of the structure
MASS CDG_X CDG_Y CDG_Z
ALL: “YES” 9.49787E+07 0.00000E+00 0.00000E+00 1.94801E+01
GROUP_MA: POU_D_T 5.55670E+05 0.00000E+00 0.00000E+00 2.95682E+01
GROUP_MA: LIAI_SOL 0.00000E+00 0.00000E+00 0.00000E+00 0.00000E+00
GROUP_MA: MASSES 9.44230E+07 0.00000E+00 0.00000E+00 1.94208E+01
GROUP_MA: LIAI_NOE 0.00000E+00 0.00000E+00 0.00000E+00 0.00000E+00
IX IY IZ IXY
ALL: “YES” 5.75518E+10 5.71540E+10 2.12362E+10 0.00000E+00
GROUP_MA: POU_D_T 1.64545E+07 1.58475E+07 1.04470E+07 0.00000E+00
GROUP_MA: LIAI_SOL 0.00000E+00 0.00000E+00 0.00000E+00 0.00000E+00
GROUP_MA: MASSES 5.74785E+10 5.70813E+10 2.12258E+10 0.00000E+00
GROUP_MA: LIAI_NOE 0.00000E+00 0.00000E+00 0.00000E+00 0.00000E+00
IXZ IYZ
ALL: “YES” - 1.84254E-08 0.00000E+00
GROUP_MA: POU_D_T - 1.84254E-08 0.00000E+00
GROUP_MA: LIAI_SOL 0.00000E+00 0.00000E+00
GROUP_MA: MASSES 0.00000E+00 0.00000E+00
GROUP_MA: LIAI_NOE 0.00000E+00 0.00000E+00
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Titrate:
Operator
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Key
:
U4.81.22-G1
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4.2
Calculation of the potential energy of modes 1, 2 and 7
·
for all the structure (
ALL = “YES”
)
·
for the group of meshs containing the beams (
GROUP_MA = “pou_d_t'
)
·
for the group of meshs containing the connections on the ground (
GROUP_MA = “liai_sol”
)
·
for the group of meshs containing the additional masses (
GROUP_MA = “masses”
)
·
for the group of meshs containing the connections between nodes (
GROUP_MA = “liai_noe”
)
·
for the meshs (
MAILLE= “E101”
with
“E2601”
)
·
for the meshs (
MAILLE= “ELN1”
with
“ELN5”
)
Order
enerpot = POST_ELEM (RESULTAT= modes, MODELE= stickmod,
NUME_MODE= (1,2,7,),
CHAM_MATER= chmater, CARA_ELEM= caraelem,
ENER_POT = _F (TOUT= “YES”,
GROUP_MA= (“pou_d_t', “liai_sol”, “masses”, “liai_noe”,),
MAILLE= (“E101”, “E201”, “E301”, “E401”, “E501”, “E601”,
“E701”, “E801”, “E901”, “E1001”, “E1101”, “E1201”,
“E1301”, “E1401”, “E1501”, “E1601”, “E1701”, “E1801”,
“E1901”, “E2001”, “E2101”, “E2201”, “E2301”, “E2401”,
“E2501”, “E2601”,
“ELN1”, “ELN2”, “ELN3”, “ELN4”, “ELN5”),),
TITER= “potential energies of modes 1, 2 and 7”,
)
Impression on the file
“RESULT”
----------------------------------------------------------------------------
potential energies of modes 1, 2 and 7
COUNT
0 ENERPOT_CHAM_ELEM! ==> TABLE cap containing a table of CHAM_ELEM
1 ENERPOT_NUME_00001! and tables of result of modes 1, 2 and 7
2 ENERPOT_NUME_00002!
7 ENERPOT_NUME_00007!
----->
CONCEPT ENERPOT OF THE TYPE TABL_ENER_POT CALCULATES FROM THE CONCEPT MODES
COUNT: ENERPOT_CHAM_ELEM RESULTING FROM TABLE ENERPOT
CHAM_ELEM
1 ENERPOT_C_NU_00001! ==> TABLE of CHAM_ELEM containing the fields of
2 ENERPOT_C_NU_00002! distribution of energy on all them
7 ENERPOT_C_NU_00007! meshs of the structure
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:
U4.81.22-G1
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HT-62/06/004/A
----->
CONCEPT ENERPOT OF THE TYPE TABL_ENER_POT CALCULATES FROM THE CONCEPT MODES
FIELD: ENERPOT_C_NU_00001 RESULTING FROM TABLE ENERPOT_CHAM_ELEM
NUME_MODE: 1 FREQ: 3.95868E+00! ==> impression of the percentage
! of distribution of energy
(Distribution of the deformation energy in various meshs)
TOTAL E101 TRAC_COM TORSION FLEX_Y FLEX_Z!all meshs
1 1.80451E-02 0. 0. 1.80451E-02 0. !for mode 1
---------- ! a certain number of omitted lines -------------------------
TOTAL E2601 TRAC_COM TORSION FLEX_Y FLEX_Z
1 4.06820E-04 0. 0. 4.06820E-04 0.
TOTAL MAS1 DX DY DZ DRX DRY DRZ
---------- ! a certain number of omitted lines -------------------------
1 0. 0. 0. 0. 0. 0. 0.
TOTAL MAS27 DX DY DZ DRX DRY DRZ
1 0. 0. 0. 0. 0. 0. 0.
TOTAL SOL1 DX DY DZ DRX DRY DRZ
1 2.69881E-01 0. 5.20243E-02 0. 2.17857E-01 0. 0.
TOTAL ELN1 DX DY DZ DRX DRY DRZ
1 3.14406E-04 0. 3.14330E-04 0. 7.62943E-08 0. 0.
TOTAL ELN2 DX DY DZ DRX DRY DRZ
1 5.09467E-05 0. 3.55125E-05 0. 1.54342E-05 0. 0.
TOTAL ELN3 DX DY DZ DRX DRY DRZ
1 3.02716E-04 0. 1.72250E-04 0. 1.30466E-04 0. 0.
TOTAL ELN4 DX DY DZ DRX DRY DRZ
1 2.14163E-04 0. 2.37436E-05 0. 1.90419E-04 0. 0.
TOTAL ELN5 DX DY DZ DRX DRY DRZ
1 5.19557E-04 0. 4.56885E-04 0. 6.26719E-05 0. 0.
----->
CONCEPT ENERPOT OF THE TYPE TABL_ENER_POT CALCULATES FROM THE CONCEPT MODES
COUNT: ENERPOT_NUME_00001 RESULTING FROM TABLE ENERPOT
NUME_MODE: 1 FREQ: 3.95868E+00! impr of the TABLE of energy
TOTAL POUR_CENT! potential for mode 1:
ALL: “YES” 7.72292E+09 1.00000E+02! total energy and percentage
GROUP_MA: POU_D_T 5.62782E+09 7.28717E+01!
GROUP_MA: LIAI_SOL 2.08427E+09 2.69881E+01
GROUP_MA: MASSES 0. 0.
GROUP_MA: LIAI_NOE 1.08259E+07 1.40179E-01
NET: E101 1.39361E+08 1.80451E+00
---------- ! a certain number of omitted lines -------------------------
NET: E2601 3.14184E+06 4.06820E-02
NET: ELN1 2.42813E+06 3.14406E-02
NET: ELN2 3.93457E+05 5.09467E-03
NET: ELN3 2.33785E+06 3.02716E-02
NET: ELN4 1.65396E+06 2.14163E-02
NET: ELN5 4.01250E+06 5.19557E-02
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Titrate:
Operator
POST_ELEM
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Key
:
U4.81.22-G1
Page:
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Instruction manual
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HT-62/06/004/A
4.3
Calculation of the kinetic energy of modes 1, 2 and 7
·
for all the structure (
TOUT= “YES”
)
·
for the group of meshs containing the beams (
GROUP_MA = “POU_D_T'
)
·
for the group of meshs containing the connections on the ground (
GROUP_MA = “LIAI_SOL”
)
·
for the group of meshs containing the additional masses (
GROUP_MA = “MASSES”
)
·
for the group of meshs containing the connections between nodes (
GROUP_MA = “LIAI_NOE”
)
·
for the meshs (
NET = “MAS1”
with
“MAS27”
)
·
for the meshs (MESH =
'
E2001
'
,
'
E2101
'
,
'
E2201
'
)
Order
enercin = POST_ELEM (RESULTAT= modes, MODELE= stickmod,
NUME_MODE= (1,2,7,),
CHAM_MATER= chmater, CARA_ELEM= caraelem,
ENER_CIN= _F (TOUT= “YES”,
GROUP_MA= (“pou_d_t', “liai_sol”, “masses”, “liai_noe”,),
MAILLE= (“MAS1”, “MAS2”, “MAS3”, “MAS4”, “MAS5”, “MAS6”,
“MAS7”, “MAS8”, “MAS9”, “MAS10”, “MAS11”, “MAS12”,
“MAS13”, “MAS14”, “MAS15”, “MAS16”, “MAS17”, “MAS18”,
“MAS19”, “MAS20”, “MAS21”, “MAS22”, “MAS23”, “MAS24”,
“MAS25”, “MAS26”, “MAS27”,
“E2001”, “E2101”, “E2201”),),
TITER= “kinetic energies of modes 1, 2 and 7”,
)
Impression on the file
“RESULT”
:
------------------------------------------------------------------
kinetic energies of modes 1, 2 and 7
COUNT
0 ENERCIN_CHAM_ELEM! ==> TABLE cap containing a table of CHAM_ELEM
1 ENERCIN_NUME_00001! and tables of result of modes 1, 2 and 7
2 ENERCIN_NUME_00002!
7 ENERCIN_NUME_00007!
CONCEPT ENERCIN OF THE TYPE TABL_ENER_CIN CALCULATES FROM THE CONCEPT MODES
COUNT: ENERCIN_CHAM_ELEM RESULTING FROM TABLE ENERCIN
CHAM_ELEM
1 ENERCIN_C_NU_00001! ==> TABLE of CHAM_ELEM containing the fields of
2 ENERCIN_C_NU_00002! distribution of energy on all them
7 ENERCIN_C_NU_00007! meshs of the structure
----->
CONCEPT ENERCIN OF THE TYPE TABL_ENER_CIN CALCULATES FROM THE CONCEPT MODES
FIELD: ENERCIN_C_NU_00001 RESULTING FROM TABLE ENERCIN_CHAM_ELEM
NUME_MODE: 1 FREQ: 3.95868E+00! ==> impression of the percentage
! of distribution of energy
TOTAL E101 DX DY DZ DRX DRY DRZ! on all the meshs
1 0. 0. 0. 0. 0. 0. 0. ! for mode 1
TOTAL E201 DX DY DZ DRX DRY DRZ
1 0. 0. 0. 0. 0. 0. 0.
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Titrate:
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POST_ELEM
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Key
:
U4.81.22-G1
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Instruction manual
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HT-62/06/004/A
---------- ! a certain number of omitted lines -------------------------
TOTAL E2501 DX DY DZ DRX DRY DRZ
1 0. 0. 0. 0. 0. 0. 0.
TOTAL E2601 DX DY DZ DRX DRY DRZ
1 0. 0. 0. 0. 0. 0. 0.
TOTAL E2001 DX DY DZ DRX DRY DRZ
1 8.74690E-04 0. 8.73486E-04 0. 0. 0. 1.20387E-06
TOTAL E2101 DX DY DZ DRX DRY DRZ
1 1.47949E-03 0. 1.47806E-03 0. 0. 0. 1.43435E-06
TOTAL E2201 DX DY DZ DRX DRY DRZ
1 8.74196E-04 0. 8.73476E-04 0. 0. 0. 7.20094E-07
TOTAL MAS1 DX DY DZ DRX DRY DRZ
1 9.45582E-04 0. 4.03156E-04 0. 5.42426E-04 0. 0.
TOTAL MAS2 DX DY DZ DRX DRY DRZ
1 1.62612E-03 0. 9.06238E-04 0. 7.19885E-04 0. 0.
---------- ! a certain number of omitted lines -------------------------
TOTAL MAS26 DX DY DZ DRX DRY DRZ
1 1.92897E-03 0. 1.92897E-03 0. 0. 0. 0.
TOTAL MAS27 DX DY DZ DRX DRY DRZ
1 8.12621E-04 0. 8.12621E-04 0. 0. 0. 0.
TOTAL SOL1 DX DY DZ DRX DRY DRZ
1 0. 0. 0. 0. 0. 0. 0.
---------- ! a certain number of omitted lines -------------------------
TOTAL ELN4 DX DY DZ DRX DRY DRZ
1 0. 0. 0. 0. 0. 0. 0.
TOTAL ELN5 DX DY DZ DRX DRY DRZ
1 0. 0. 0. 0. 0. 0. 0.
----->
CONCEPT ENERCIN OF THE TYPE TABL_ENER_CIN CALCULATES FROM THE CONCEPT MODES
COUNT: ENERCIN_NUME_00001 RESULTING FROM TABLE ENERCIN
NUME_MODE: 1 FREQ: 3.95868E+00! impression of the TABLE of energy
TOTAL POUR_CENT! kinetics for mode 1:
ALL: “YES” 7.72292E+09 1.00000E+02! total energy and percentage
GROUP_MA: POU_D_T 2.49325E+07 3.22838E-01!
GROUP_MA: LIAI_SOL 0. 0.
GROUP_MA: MASSES 7.69798E+09 9.96772E+01
GROUP_MA: LIAI_NOE 0. 0.
NET: MAS1 7.30265E+06 9.45582E-02
NET: MAS2 1.25584E+07 1.62612E-01
NET: MAS3 1.92226E+07 2.48904E-01
---------- ! a certain number of omitted lines -------------------------
NET: E2001 6.75516E+06 8.74690E-02
NET: E2101 1.14260E+07 1.47949E-01
NET: E2201 6.75134E+06 8.74196E-02
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Code_Aster
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Version
8.2
Titrate:
Operator
POST_ELEM
Date:
22/02/06
Author (S):
X. DESROCHES, L. VIVAN
Key
:
U4.81.22-G1
Page:
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Instruction manual
U4.8- booklet: Postprocessing and dedicated analyzes
HT-62/06/004/A


























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