List of Variables and Responses

* --- Truss (2)

1 initial cross section TAREA

* --- beam (3)

1 cross section BAREA

2 Ixx IXX

3 Iyy IYY

4 Izz IZZ

* --- spring (4) not implemented

1 Mass MASS

2 TX K (stiffness) (#) TX_K

3 TX C (damping) TX_C

4 TX A Coeff.(*) TX_A

5 TX B Coeff.(*) TX_B

6 TX D Coeff.(*) TX_D

7 TX f(x) Scale Fact.(*) TX_FX_SF

8 TX g(dx) Scale Fact.(*)(**) TX_GDX_SF

9 TX fN3 Scale Fact.(*)(#)(&) TX_FN3_SF

10 TX Neg.Rupt.Lim. TX_DELTAMIN

11 TX Pos.Rupt.Lim. TX_DELTAMAX

(*): Not available if N1 = 0

(**): Not available if N2 = 0

(#): Not available if H = 0

(&): Not available if H=1 or H=2

* --- general spring (8) not implemented

* --- beam type spring (13)

1 Mass MASS

2 Inertia INERTIA

3 TX K (stiffness) (#) TX_K

4 TX C (damping) TX_C

5 TX A Coeff.(*) TX_A

6 TX B Coeff.(*) TX_B

7 TX D Coeff.(*) TX_D

8 TX f(x) Scale Fact.(*) TX_FX_SF

9 TX g(dx) Scale Fact.(*)(**) TX_GDX_SF

10 TX fN3 Scale Fact.(*)(#)(&) TX_FN3_SF

11 TX Neg.Rupt.Lim. TX_DELTAMIN

12 TX Pos.Rupt.Lim. TX_DELTAMAX

...Idem for TY, TZ, RX, RY, RZ

(*): Not available if N1 = 0

(**): Not available if N2 = 0

(#): Not available if H = 0

(&): Not available if H=1 or H=2

* --- 3 node spring (12) not implemented

* --- X elements (28) not implemented

* --- Pretensioner spring (32) not implemented

* --- Joint type spring (33) not implemented

* --- shell (1)

1 thickness THICK

* --- orthotropic shell (9)

1 thickness THICK

* --- composite shell (10) not implemented

* --- sandwich shell (11) not implemented

* --- Orthotropic solid (6) not implemented

* --- general solid (14) not implemented

* --- Linear elastic (1)

1 initial density RHO_I

2 E E

3 nu NU

* --- Johnson-Cook (2)

1 initial density RHO_I

2 E E

3 nu NU

4 yield stress A

5 hardening param B

6 hardening exponent N

7 failure plastic strain EPSILON_MAX

8 max stress SIGMA_MAX

9 strain rate coeff C

10 ref strain rate EPS_._0

11 Cutoff Frequency F_CUT

12 Temperature Exp. M

13 Melting Temp. T_MELT

14 Specific Heat/Vol. RHO_CP

15 Initial Temp. T_I

* --- Zerilli armstrong (2)

1 initial density RHO_I

2 E E

3 nu NU

4 yield stress C0

5 hardening parameter C5

6 hardening exponent N

7 failure plastic strain EPSILON_MAX

8 max stress SIGMA_MAX

9 strain rate coeff C1

10 ref strain rate EPS_._0

11 Cutoff Frequency F_CUT

12 C3 C3

13 C4 C4

14 Specific Heat/Vol. RHO_CP

15 Initial Temp. T_I

* --- Elasto-Plastic (3) not implemented

* --- Hydrodynamic johnson cook (4) not implemented

* --- Viscous (6) not implemented

* --- Rock-Concrete (10) not implemented

* --- Orthotropic (14) not implemented

* --- Linear elastic orthotropic (19)

1 initial density RHO_I

2 E in direction 1 E11

3 E in direction 2 E22

4 Poisson coefficient nu12

5 shear modulus 12 G12

6 shear modulus 23 G23

7 shear modulus 31 G31

8 reduction fact. on E for comp RE

* --- Drucker-Prager (21) not implemented

1 Initial Density RHO_I

2 Young Modulus E

3 Poisson Coeff. NU

4 A0 A0

5 A1 A1

6 A2 A2

7 Von Mises Limit A_MAX

8 P(mu) Scale Fact. P_MU_SCALE

9 Tensile Bulk Mod K_T

10 Min Pressure P_MIN

11 Unload.Bulk Mod B21

12 Max Compression MU_MAX

* --- Ductile Damage (22)

1 initial density RHO_I

2 Young Modulus E

3 Poisson Coefficient NU

4 yield stress A

5 hardening param B

6 hardening exponent N

7 failure plastic strain EPSILON_MAX

8 max stress SIGMA_MAX

9 Strain Rate Coeff. C

10 Ref. Strain Rate EPS_._0

11 Damage Start EPS_DAM

12 Soft. Dam. Slope E_T

* --- Ductile Damage (23) not implemented

* --- brittle (24) not implemented

* --- Orthotropic shell (25) not implemented

* --- brittle shell (27)

1 initial density RHO_I

2 E E

3 nu nu

4 yield stress A

5 hardening param B

6 hardening exponent N

7 failure plastic strain EPSILON_MAX

8 max stress SIGMA_MAX

9 Strain Rate Coeff. C

10 Ref. Strain Rate EPS_._0

11 Tensile rupt. strain 1 EPSILON_T1

12 Max strain 1 EPSILON_M1

13 Max damage 1 D_MAX1

14 Strain for elt del. 1 EPSILON_F1

15 Tensile rupt. strain 1 EPSILON_T2

16 Max strain 1 EPSILON_M2

17 Max damage 1 D_MAX2

18 Strain for elt del. 1 EPSILON_F2

* --- Honeycomb orthotropic (28) not implemented

* --- Hill orthotropic (32)

1 initial density RHO_I

2 E E

3 nu NU

4 yield stress A

5 hardening param B

6 hardening exponent N

7 failure plastic strain EPSILON_MAX

8 max stress SIGMA_MAX

9 Min. Strain Rate EPS_._0_MIN

10 Strain Rate Expon. M_32

11 Lankford P. 0 deg R00

12 Lankford P. 45 deg R45

13 Lankford P. 90 deg R90

* --- Close cell foam (33)

1 Initial Density RHO_I

2 Young Modulus E

3 Initial Air P. P0

4 Foam/Polymer density PHI

5 Init.Vol.Strain GAMMA0

6 A Yield Param.* A

7 B Yield Param.* B

8 C Yield Param.* C

9 Yield Scale Factor** SCALE33

10 E1 Coeff for Young*** E1

11 E2 Coeff for Young*** E2

12 Tangent Modulus*** E_T

13 Visc.Coeff.pure Comp.*** ETA_STAR

14 Visc.Coeff.pure Shear*** ETA0

(*): available if If = 0

(**): available if If != 0. Scale factor

of the yield curve function number If, defined in CARD2.

(***): available if K_a = 1

* --- foam (34) not implemented

* --- generalized kelvin voigt (35) not implemented

* --- Piecewise linear (36)

1 initial density RHO_I

2 E E

3 nu NU

4 Maximum plastic strain EPS_P

5 tensile rupture strain 1 EPS_T1

6 tensile rupture strain 2 EPS_T2

7 Hardening Coefficient C_HARD

8 Stiffness Scale factor(*) SCALE36

(*) Scale factor applied to all the

alfa coefficients of CARD5 and CARD6

* --- foam tabulated law (38)

Initial Density RHO_I

Minimum Tension Modulus E_0

Stiffness Scale Factor(*) SCALE38

(*) It is a scale factor applied to alpha unload of CARD5,

and to all the alpha coefficients of CARD8

* --- Generelized Maxwell Kelvin (40) not implemented

* --- HyperElastic (42) not implemented

* --- Hill orthotropic tab (43) not implemented

* --- Cowper Symond (44) not implemented

* --- Gurson material (52)

1 Initial Density RHO_I

2 Young Modulus E

3 Poisson Ratio NU

4 Yield Stress A

5 Hardening Param. B

6 Hardening Exp. N

7 CowperSymond's Param c

8 Viscoplastic Exp. p

9 q1 Tvergaard Param. q1

10 q2 Tvergaard Param. q2

11 q3 Tvergaard Param. q3

12 Gaussian Std.Dev. SN

13 Nucl.Eff.Plast.Strain EPS_N

14 Init.Void.Vol.Fraction f1

15 Nucl.Void.Vol.Fraction fN

16 Crit.VVF at Coal. fC

17 Crit.VVF at Duct.Fract. fF

*********** ADDED MASS ***************************

1 Mass MASS

*********** INITIAL VELOCITY **********************

1 X-Velocity VX

2 Y-Velocity VY

3 Z-Velocity VZ

*********** PLANE RIGID WALL *********************

1 Friction(*) FRIC

2 X Transl. TRANSL_X

3 Y Transl. TRANSL_Y

4 Z Transl. TRANSL_Z

5 X Rotation ROTATE_X

6 Y Rotation ROTATE_Y

7 Z Rotation ROTATE_Z

8 Mass(**) MASS

9 X Velocity(**) VX

10 Y Velocity(**) VY

11 Z Velocity(**) VZ

(*) available only if SLIDE=2

(**) available only for moving RW

X, Y and Z rotation are rotations of the normal

vector with point M as a fixed point.

*********** CYLINDER RIGID WALL *********************

1 Friction(*) FRIC

2 Diameter PHI

3 X Transl. TRANSL_X

4 Y Transl. TRANSL_Y

5 Z Transl. TRANSL_Z

6 Mass(**) MASS

7 X Velocity(**) VX

8 Y Velocity(**) VY

9 Z Velocity(**) VZ

(*) available only if SLIDE=2

(**) available only for moving RW

*********** PARALLELOGRAM RIGID WALL ****************

1 Friction(*) FRIC

2 Mass(**) MASS

3 X Velocity(**) VX

4 Y Velocity(**) VY

5 Z Velocity(**) VZ

(*) available only if SLIDE=2

(**) available only for moving RW

*********** SPHERE RIGID WALL ************************

1 Friction(*) FRIC

2 Diameter PHI

6 Mass(**) MASS

7 X Velocity(**) VX

8 Y Velocity(**) VY

9 Z Velocity(**) VZ

(*) available only if SLIDE=2

(**) available only for moving RW

*********** MONITORED VOLUMES ************************

(AIRBAG and COMMU types only)

For AIRBAG and COMMU types:

1 Gas Constant GAMMA

2 Volumic Viscosity MU

3 External Pressure P_EXT

4 P.Diff.to Open Vent DELTA_P_DEF

5 Vent Holes Surface A_VENT

6 Start Time for Ventin T_VEN

7 Specific Heat Cp CP

8 Scal.Fact.on Mass f. S_MASS

9 Scal.Fact.on Temp.f. S_TEMP

For COMMU type only: three more

variables per communicating airbag.

10 Com.Airb.1 DeltaPDef DELTA_P_DEF_CA1

11 Com.Airb.1 ACom A_COM_CA1

12 Com.Airb.1 TCom T_COM_CA1

13 Com.Airb.2 DeltaPDef DELTA_P_DEF_CA2

14 Com.Airb.2 ACom A_COM_CA2

15 Com.Airb.2 TCom T_COM_CA2

etc.

*********** RIGID BODIES **********************

1 Mass MASS

2 Inertia JXX JXX

3 Inertia JYY JYY

4 Inertia JZZ JZZ

5 Inertia JXY JXY

6 Inertia JYZ JYZ

7 Inertia JXZ JXZ

*********** IMPOSED VELOCITY ******************

1 Scale Factor SCALE

2 T Start TSTART

3 T Stop TSTOP

*********** IMPOSED DISPLACEMENTS *************

1 Scale Factor SCALE

2 T Start TSTART

3 T Stop TSTOP

*********** GRAVITY LOADS *********************

1 Scale Factor SCALE

*********** CONCENTRATED LOADS ****************

1 Scale Factor SCALE

*********** CONTACT INTERFACES ****************

* TYPE 3, 5 and 6:

1 Stiffn.Scale Factor STFAC

2 Friction FRIC

3 Gap GAP

4 T Start TSTART

5 T Stop TSTOP

* TYPES 7 and 11:

1 Stiffness STFAC

2 Friction FRIC

3 Gap GAP

4 T Start TSTART

5 T Stop TSTOP

* TYPE 8:

1 Drawbead Force FT

2 T Start TSTART

3 T Stop TSTOP

* TYPE 10:

1 Stiffn.Scale Factor STFAC

2 Gap GAP

3 T Start TSTART

4 T Stop TSTOP

* TYPE 14:

1 Stiffness STIF

2 Friction FRIC

3 Norm.Viscosity VISC

4 Gap GAP

* TYPE 15:

1 Stiffness STIF

2 Friction FRIC

*********** SPOTWELDS ***************************

*********** WELDING LINE ************************

*********** HEMMING *****************************

*********** GLUE ********************************

*********** BOLT with SPRING ********************

-> variables of the associated SPR_BEAM property:

1 Mass MASS

2 Inertia INERTIA

3 Traction K (stiffness) (#) TX_K

4 Traction C (damping) TX_C

5 Traction A Coeff.(*) TX_A

6 Traction B Coeff.(*) TX_B

7 Traction D Coeff.(*) TX_D

8 Traction f(x) Scale Fact.(*) TX_FX_SF

10 Traction Neg.Rupt.Lim. TX_DELTAMIN

11 Traction Pos.Rupt.Lim. TX_DELTAMAX

...Idem for Shear, Torsion and Bending.

(*): Not available if N1 = 0

(#): Not available if H = 0

Note:

For all types of connections, the stiffness is assumed to be the same in TY and TZ (shear), and in RY and RZ (bending).

1 internal E IE

2 kinetic E KE

3 x momentum XMOM

4 y momentum YMOM

5 z momentum ZMOM

6 mass MASS

7 time step DT

8 rotation E RKE

9 external work EFW

10 spring E SIE

11 contact E CE

12 hourglass E HE

13 total E TE

14 total E incl. rot E TER

15 global E TTE

16 variation of global E DTE

17 velocity x VX

18 velocity y VY

19 velocity z VZ

1 internal E IE

2 kinetic E KE

3 x momentum XMOM

4 y momentum YMOM

5 z momentum ZMOM

6 mass MASS

7 hourglass E HE

8 rotation E RKE

9 total E TE

10 velocity x VX

11 velocity y VY

12 velocity z VZ

1 X Displacement DX

2 Y Displacement DY

3 Z Displacement DZ

4 X Velocity VX

5 Y Velocity VY

6 Z Velocity VZ

7 X Acceleration AX

8 Y Acceleration AY

9 Z Acceleration AZ

10 X Coordinate X

11 Y Coordinate Y

12 Z Coordinate Z

13 Magnitude of Disp DISP

14 Magnitude of Velocity VEL

15 Magnitude of Accel ACC

16 Angle btw DX and DY ADXY

17 Angle btw DY and DZ ADYZ

18 Angle btw DX and DZ ADZX

19 Angle btw VX and VY AVXY

20 Angle btw VY and VZ AVYZ

21 Angle btw VX and VZ AVZX

22 Angle btw AX and AY AAXY

23 Angle btw AY and AZ AAYZ

24 Angle btw AX and AZ AAZX

*********** BRICK *****************************

1 Stress X SX

2 Stress Y SY

3 Stress Z SZ

4 Shear Stress XY SXY

5 Shear Stress YZ SYZ

6 Shear Stress XZ SXZ

7 Local Stress X LSX

8 Local Stress Y LSY

9 Local Stress Z LSZ

10 Local Shear Stress XY LSXY

11 Local Shear Stress YZ LSYZ

12 Local Shear Stress XZ LSXZ

13 Internal Energy IE

14 Density DENS

15 Bulk Viscosity P BULK

16 Element Volume VOL

17 Pressure P

18 Von Mises Stress VONM

*********** SHELL / TRIANGLE ******************

1 Mean stress dir 1 F1

2 Mean stress dir 2 F2

3 Mean stress dir 12 F12

4 Mean stress dir 13 Q1

5 Mean stress dir 23 Q2

6 Moment / L*thick^2 dir 1 M1

7 Moment / L*thick^2 dir 2 M2

8 Moment / L*thick^2 dir 12 M12

9 Membrane Energy IEM

10 Bending Energy IEB

11 Thickness THIC

12 Min.plast.strain over int.pts EMIN

13 Max.plast.strain over int.pts EMAX

14 Membrane strain dir.1 E1

15 Membrane strain dir.2 E2

16 Membrane strain dir.12 E12

17 Shear strain dir.1 SH1

18 Shear strain dir.2 SH2

19 Curvature dir 1 K1

20 Curvature dir 2 K2

21 Curvature dir 12 K12

22 Pressure P

23 Von Mises Strain VONM

*********** SPRINGS ***************************

1 Force X FX

2 Force Y FY

3 Force Z FZ

4 Moment X MX

5 Moment Y MY

6 Moment Z MZ

7 Elongation X LX

8 Elongation Y LY

9 Elongation Z LZ

10 Rotation X RX

11 Rotation Y RY

12 Rotation Z RZ

13 Internal Energy IE

14 Magn. of Force F

15 Magn. of Moment M

16 Magn. of Elongation L

17 Magn. of Rotation R

*********** BEAM ******************************

1 Normal Force 1 F1

2 Shear Force 12 F2

3 Shear Force 13 F3

4 Torsional Moment M1

5 Bending Moment 12 M2

6 Bending Moment 13 M3

7 Internal Energy IE

8 Shear Force FT

*********** TRUSS *****************************

1 Normal Force F

2 Internal Energy IE

3 Normal Section A

4 Initial length L

*********** SECTION ***************************

1 Normal Force X FNX

2 Normal Force Y FNY

3 Normal Force Z FNZ

4 Tangential Force X FTX

5 Tangential Force Y FTY

6 Tangential Force Z FTZ

7 Moment in dir 1 M1

8 Moment in dir 2 M2

9 Moment in dir 3 M3

10 Normal Force Magn. NF

11 Tangential Force Magn. TF

12 Moment Magn. TM

13 Force X FX

14 Force Y FY

15 Force Z FZ

*********** ACCELEROMETERS ********************

1 Accel.X AX

2 Accel.Y AY

3 Accel.Z AZ

4 Accel.Magn. ACC

*********** RIGID WALL ************************

1 Normal Force X FNX

2 Normal Force Y FNY

3 Normal Force Z FNZ

4 Tangential Force X FTX

5 Tangential Force Y FTY

6 Tangential Force Z FTZ

10 Normal Force Magn. NF

11 Tangential Force Magn. TF

*********** RIGID BODIES **********************

1 Rotation X RX

2 Rotation Y RY

3 Rotation Z RZ

4 Force X FX

5 Force Y FY

6 Force Z FZ

7 Moment X MX

8 Moment Y MY

9 Moment Z MZ

10 Force Magnitude TF

11 Moment Magnitude TM

*********** MONITORED VOLUMES *****************

1 Mass MASS

2 Volume VOL

3 Pressure P

4 Area A

5 Temperature T

6 Vent Area AO

7 Vent Velocity UO

*********** CONTACT INTERFACES ****************

1 Normal Force X FNX

2 Normal Force Y FNY

3 Normal Force Z FNZ

4 Tangential F. X FTX

5 Tangential F. Y FTY

6 Tangential F. Z FTZ

7 Normal F.Magn. NF

8 Tangent. F.Magn. TF