/FAIL/SNCONNECT
Block Format Keyword Describes the failure model for CONNECTION material with plastic displacement criteria. This model allows a different failure behavior in normal and shear directions.
Format
(1)  (2)  (3)  (4)  (5)  (6)  (7)  (8)  (9)  (10) 

/FAIL/SNCONNECT/mat_ID/unit_ID  
${\alpha}_{0}$  ${\beta}_{0}$  ${\alpha}_{f}$  ${\beta}_{f}$  Ifail_so  ISYM  
fct_ID_{0N}  fct_ID_{0S}  fct_ID_{FN}  fct_ID_{FS}  XSCALE_0  XSCALE_F  AREA_{scale} 
(1)  (2)  (3)  (4)  (5)  (6)  (7)  (8)  (9)  (10) 

fail_ID 
Definition
Field  Contents  SI Unit Example 

mat_ID  Material identifier. (Integer, maximum 10 digits) 

unit_ID  Unit Identifier. (Integer, maximum 10 digits) 

${\alpha}_{0}$  Parameter for the beginning of
damage, due to moment loads. 2 (Real) 

${\beta}_{0}$  Exponent for the beginning of damage,
due to combined shear and normal loads. 2 (Real) 

${\alpha}_{f}$  Parameter for the final damage failure,
due to moment loads. 2 (Real) 

${\beta}_{f}$  Exponent for the final damage failure,
due to combined shear and normal loads. 2 (Real) 

Ifail_so  Solid failure flag.
(Integer) 

ISYM  Rupture deactivation flag for compression.
(Integer) 

fct_ID_{0N}  Function identifier defining a scale
factor for displacement rate dependency in normal direction in initial yield
function. Default = 0 (Integer) 

fct_ID_{0S}  Function identifier defining a scale
factor for displacement rate dependency in tangential direction in initial yield
function. Default = 0 (Integer) 

fct_ID_{FN}  Function identifier defining a scale
factor for displacement rate dependency in normal direction in rupture yield
function. Default = 0 (Integer) 

fct_ID_{FS}  Function identifier defining a scale
factor for displacement rate dependency in tangential direction in rupture yield
function. Default = 0 (Integer) 

XSCALE_0  Scale factor for the abscissa
displacement rate for initial function. Default = 1.0 (Real) 
$\left[\frac{\text{1}}{\text{s}}\right]$ 
XSCALE_F  Scale factor for the abscissa
displacement rate for rupture function. Default = 1.0 (Real) 
$\left[\frac{\text{1}}{\text{s}}\right]$ 
AREA_{scale}  Failure scale factor for area
increase. 5 Default = 0.0, this option is not used (Real) 

fail_ID  Failure
criteria identifier. 3 (Integer, maximum 10 digits) 
Example (Connect)
#RADIOSS STARTER
#12345678910
/UNIT/1
unit for mat
kg mm ms
#12345678910
# 2. MATERIALS:
#12345678910
/MAT/LAW83/1/1
CONNECT MATERIAL
# RHO_I
7.8E6
# E Imass
20 0
# Fct_ID1 Y_scale1 X_scale1 ALPHA BETA
200 1 1 0 2
# RN RS Fsmooth Fcut
.2 .4 0 0
# Fct_IDN Fct_IDS XSCALE
0 0 0
/FAIL/SNCONNECT/1/1
# ALPHA_0 BETA_0 ALPHA_F BETA_F Ifail_so ISYM
0 2 0 2 1 1
# Fct_0N Fct_0S Fct_FN Fct_FS XSCALE_0 XSCALE_F AREAscale
2001 2002 2003 2004 1 1 0
#12345678910
# 3. FUNCTIONS:
#12345678910
/FUNCT/200
MAT83 curve
# X Y
0 1
1 1
#12345678910
/FUNCT/2001
Fct_0N
# X Y
0 .5
1 .5
#12345678910
/FUNCT/2002
Fct_0S
# X Y
0 .5
1 .5
#12345678910
/FUNCT/2003
Fct_fN
# X Y
0 1
1 1
#12345678910
/FUNCT/2004
Fct_fS
# X Y
0 1
1 1
#12345678910
#ENDDATA
/END
#12345678910
Comments
 This failure model is compatible only with the connection materials, /MAT/LAW59 (CONNECT) and /MAT/LAW83. The connection materials are independent of height, so failure is based on displacement, instead of strain.
 A combined energy failure criteria is
defined as:
Where, ${\overline{u}}_{n}{}^{pl}$ and ${\overline{u}}_{s}{}^{pl}$ are the plastic displacement in the normal and tangential directions.
Damage of element begins when the damage surface is reached which is described by:(1) $$1={\left[{\left(\frac{{\overline{u}}_{0,n}^{pl}}{{\mathrm{f}}_{0N}\left(1{\alpha}_{0}\cdot sym\right)}\right)}^{{\beta}_{0}}+{\left(\frac{{\overline{u}}_{0,s}^{pl}}{{\mathrm{f}}_{0S}}\right)}^{{\beta}_{0}}\right]}^{\frac{1}{{\beta}_{0}}}$$Where, ${\mathrm{f}}_{0N}$ and ${\mathrm{f}}_{0S}$ are the function of fct_ID_{0N} and fct_ID_{0S}. If there are no rate effects, the curves will be constant.
The damage factor is computed as:(2) $$d=\frac{{\overline{u}}^{pl}{\overline{u}}_{0}^{pl}}{{\overline{u}}_{f}^{pl}{\overline{u}}_{0}^{pl}}$$And the stress is reduced as:(3) $$\sigma =\sigma \left(1d\right)$$The element is deleted when the rupture surface is reached:(4) $$1={\left[{\left(\frac{{\overline{u}}_{f,n}^{pl}}{{\mathrm{f}}_{FN}\left(1{\alpha}_{f}\cdot sym\right)}\right)}^{{\beta}_{f}}+{\left(\frac{{\overline{u}}_{f,s}^{pl}}{{\mathrm{f}}_{FS}}\right)}^{{\beta}_{f}}\right]}^{\frac{1}{{\beta}_{f}}}$$Where, ${\mathrm{f}}_{FN}$ and ${\mathrm{f}}_{FS}$ are the function of fct_ID_{FN} and fct_ID_{FS}. If there are no rate effects, the curves will be constant.

$sym=\mathrm{sin}(A)$
.Where, $A$ is the angle between the normal of the lower surface and the normal of the upper surface of the solid element.
 Parameters ${\alpha}_{0},{\alpha}_{f}$ are the scale factors used to describe the moment effect (for example, in a peeling test) for damage initiation and failure.
 Parameters ${\beta}_{0},{\beta}_{f}$ are fitted using a test which combines normal and shear loards (30° test, 45° test or 60° test, etc.). At least one combined test is needed to fit the parameters ${\beta}_{0},{\beta}_{f}$ . Figure 3 and Figure 4 show the effect of ${\beta}_{0},{\beta}_{f}$ on damage initiation and failure in combined test.

$sym=\mathrm{sin}(A)$
.
 The fail_ID is used with /STATE/BRICK/FAIL and /INIBRI/FAIL. There is no default value. If the line is blank, no value will be output for failure model variables in the /INIBRI/FAIL (written in .sta file with /STATE/BRICK/FAIL option).
 With /ANIM/BRICK/VDAMi following damage variable value could be output in
an animation file:
VDAM1 = d is the damage value, which ranges from [0, 1].
VDAM2 = the damage surface output, which ranges from [0, 1].
VDAM3 = the rupture surface output, which ranges from [0, 1].
 The area is calculated as the mean value of the upper and lower surface of the solid element. If the actual area reaches the value of initial area multiplied by the AREA_{scale} factor, the whole element will be deleted. The default value is set to zero. This causes no deletion, due to area increase. The application is to prevent shooting nodes, if the cohesive element nodes will be released, when surrounding elements start to fail and erode.