Full law name : SILCOETC3D
Coupled plastic-damage multiracial constitutive law for concrete behaviour.
For further details see PhD thesis of Thomas Gernay or Andra report by B. Cerfontaine.
Prepro: LSILCOETC3D.F
Lagamine: PIL_SILCOET3D.F
Plane stress state | NO |
Plane strain state | YES |
Axisymmetric state | NO |
3D state | YES |
Generalized plane state | NO |
Line 1 (2I5, 60A1) | |
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IL | Law number |
ITYPE | 618 |
COMMNT | Any comment (up to 60 characters) that will be reproduced on the output listing |
Line 1 (6I5) | |
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NINTV | = 0 : By default |
ISOL | = 0 : Use of total stresses in the constitutive law |
≠ 0 : Use of effective stresses in the constitutive law (See annex 7) | |
KMETH | = 2 : Actualised vgrad method |
= 3 : Mean vgrad method (default) | |
ITEMP | $n$ = 0 : Influence of temperature (not yet activated) (by default) |
ICREEP | = 0 : Introduction of creep (not yet activated) (by default) |
IHYDR | = 0 : Early age behaviour (not yet activated) (by default) |
Line 1 (5G10.0) | |
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fc | Uniaxial compression strength |
ft | Uniaxial tension strength |
fc0 | Uniaxial compression elastic limit (by default = 0.3fc) |
fb | Biaxial strength (by default = 1.16fc) |
$\varepsilon_{peak}$ | Total deformation at peak stress for uniaxial compression |
Line 2 (4G10.0) | |
ANU | POISSON's ratio |
E | YOUNG's elastic modulus |
DIV | DIV parameter |
RHO | Specific mass |
Line 3 (4G10.0) | |
$\alpha$g | Dilatancy parameters |
dc | Damage at peak stress for uniaxial compression |
gt | Crack energy density per unit volume [Nm/m$^2$] |
xc | Ratio between crack energy dissipated before peak and total energy dissipated |
If ICREEP == 1 :
Line 4 (XG10.0) | |
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X | Creep parameters |
If IHYDR == 1 :
Line 5 (4G10.0) | |
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ALPHATH | Hydration threshold (properties are equal to Eth/E0) |
Pa | Parameter for the evolution of strength |
Pb | Parameter for the evolution of stiffness |
Eth | Elastic stiffness below threshold |
Note : The evolution of the hydration degree must be specified in file .hydr such that :
TIMES |
(I10) Number of time steps defined below |
(2G10.0,repeated) Time step, alpha |
6 for 3D state
4 for the other cases
The stresses are the components of CAUCHY stress tensor in global (X,Y,Z) coordinates.
For the 3-D state:
SIG(1) | $\sigma_{xx}$ |
SIG(2) | $\sigma_{yy}$ |
SIG(3) | $\sigma_{zz}$ |
SIG(4) | $\sigma_{xy}$ |
SIG(5) | $\sigma_{xz}$ |
SIG(6) | $\sigma_{yz}$ |
For the other cases:
SIG(1) | $\sigma_{xx}$ |
SIG(2) | $\sigma_{yy}$ |
SIG(3) | $\sigma_{xy}$ |
SIG(4) | $\sigma_{zz}$ |
44
Q(1) | Element thickness ($t$) in plane stress state |
= 1 : Plane strain state | |
Circumferential strain rate ($\varepsilon_r$) in axisymmetrical state | |
= 0 : 3D state | |
Element thickness ($t$) in generalized plane state | |
Q(2) | Nothing |
Q(3) | Volumetric deformation |
Q(4-9) | Total strain (mechanical + transient) |
Q(10-15) | Mechanical strain |
Q(16-21) | Transient creep strain |
Q(22-27) | Plastic strain |
Q(29-30) | Damage : dt, dc |
Q(31-32) | Internal variables : kt, kc |
Q(33-38) | Effective stress |
Q(39-44) | Compressive part of the effective stress |