/ANIM/BRICK/Restype

Engine Keyword Generates animation files containing brick element data for the specified result. Options used for BRICK element type.

Format

/ANIM/Eltyp/Restype

Definition

Field Contents SI Unit Example
Eltyp Element type.
ELEM
BRICK
Brick elements
 
Restype
AMS
Elements using AMS timestep due to /DT/CST_AMS.
BFRAC
Burn fraction.
COLOR
1*vfrac1 + 2*vfrac2 + .... + last*vfracN (LAW51 and LAW151 only).
DAM1 , DAM2 or DAM3
Damage in direction 1, 2 or 3. 9
DAMG
Mean damage value over integration points (only for coupled damage models). 11
DENS
Density
DT
Element time step. 10
EINT
Internal energy.
ENER
Specific energy (internal energy divided by the element mass).
EPSD
Equivalent strain rate in bricks and in shells too (only available in case of strain rate filtering).
EPSP
Plastic strain ε p .
FILL
Filling percentage. This option is used only with Eltyp =BRICK for /INIBRI/FILL.
FIN
Cell internal Forces for FVM with /INTER/TYPE22 for all components and magnitude.
To request each separately use: FINX, FINY, FINZ, FINXY, FINYZ, FINXZ, |FIN|.
HOURG
Hourglass energy per mass unit
K
Turbulent energy for ALE material law.
LAW51
Display results for all Sub-material or specific Sub-material. 8
MACH
Mach number (/MAT/LAW151 (MULTIFLUID) only).
MOM
Cell momentum Density (MOM) for FVM with /INTER/TYPE22 for all components and magnitude.
To request each separately use: MOMX, MOMY, MOMZ, MOMXY, MOMYZ, MOMXZ, |MOM|.
NL_EPSD
Non-local plastic strain rate ε ˙ p n l MathType@MTEF@5@5@+= feaahqart1ev3aaatCvAUfeBSjuyZL2yd9gzLbvyNv2CaerbuLwBLn hiov2DGi1BTfMBaeXatLxBI9gBaerbd9wDYLwzYbItLDharqqtubsr 4rNCHbGeaGqiVu0Je9sqqrpepC0xbbL8F4rqqrFfpeea0xe9Lq=Jc9 vqaqpepm0xbba9pwe9Q8fs0=yqaqpepae9pg0FirpepeKkFr0xfr=x fr=xb9adbaqaaeGaciGaaiaabeqaamaabaabaaGcbaGafqyTduMbai aadaqhaaWcbaGaamiCaaqaaiaad6gacaWGSbaaaaaa@3AA9@ (only if /NONLOCAL/MAT is activated). 12
NL_EPSP
Non-local plastic strain ε p n l MathType@MTEF@5@5@+= feaahqart1ev3aaatCvAUfeBSjuyZL2yd9gzLbvyNv2CaerbuLwBLn hiov2DGi1BTfMBaeXatLxBI9gBaerbd9wDYLwzYbItLDharqqtubsr 4rNCHbGeaGqiVu0Je9sqqrpepC0xbbL8F4rqqrFfpeea0xe9Lq=Jc9 vqaqpepm0xbba9pwe9Q8fs0=yqaqpepae9pg0FirpepeKkFr0xfr=x fr=xb9adbaqaaeGaciGaaiaabeqaamaabaabaaGcbaGaeqyTdu2aa0 baaSqaaiaadchaaeaacaWGUbGaamiBaaaaaaa@3AA0@ (only if /NONLOCAL/MAT is activated). 12
OFF
Element status.
Where,
= -1
Element is not active (it is defined in an activated rigid body).
= 0
Deleted element.
Between 0 and 1
Under failure process.
= 1
Active element.
ORTHDIR/I
Euler angles ( ψ , θ , and ϕ in unit [ deg ] in layer I).
ORTHDIR/ALL
Euler angles ( ψ , θ , and ϕ in unit [ deg ] in all layers)
Defining orthotropic reference system with global reference system - only for orthotropic solid properties. 2
P
Pressure
QVIS
Displays artificial viscous pressure
SCHLIEREN
Schlieren image (optical method widely used in CFD field). Only available with ALE material laws. 7
SIGEQ
Equivalent stress, based on the yield criteria used for the corresponding material. 3
SIGX
Stress XX 5
SIGY
Stress YY
SIGZ
Stress ZZ
SIGXY
Shear stress XY
SIGYZ
Shear stress YZ
SIGZX
Shear stress ZX
SSP
Sound speed. Only available with ALE material laws.
TDET
Detonation times for high explosive JWL EOS.
TEMP
Temperature
TILLOTSON
Region identifier for Tillotson Equation of State (/EOS/TILLOTSON).
TSAIWU
Tsai Wu criterion for /MAT/LAW12 (3D_COMP), /MAT/LAW14 (COMPSO) and /MAT/LAW25 (COMPSH).
TVIS
Turbulent viscosity for ALE material law.
USRi
User law variable ( i MathType@MTEF@5@5@+= feaagKart1ev2aaatCvAUfeBSjuyZL2yd9gzLbvyNv2CaerbuLwBLn hiov2DGi1BTfMBaeXatLxBI9gBaerbd9wDYLwzYbItLDharqqtubsr 4rNCHbGeaGqiVu0Je9sqqrpepC0xbbL8F4rqqrFfpeea0xe9Lq=Jc9 vqaqpepm0xbba9pwe9Q8fs0=yqaqpepae9pg0FirpepeKkFr0xfr=x fr=xb9adbaqaaeGaciGaaiaabeqaamaabaabaaGcbaGaamyAaaaa@36E4@ =1 to 18).
USRII
User law variable on each integration points (II =1 to 99 number of the variable). 6
Tip: Since the number of user variables that can be output is limited, use /H3D/SOLID/USER/ instead.
VEL
Cell velocity for FVM with /INTER/TYPE22 for all components and magnitude.
To request each separately use: VELX, VELY, VELZ, VELXY, VELYZ, VELXZ, |VEL|.
VFRAC
All volumetric fractions (for ALE multi-material laws: LAW20, LAW37, LAW51 and LAW151).
VONM
von Mises stress
VORTX
Vorticity around x for QUAD (2D) and SOLID (3D) with ALE material law.
VORTY
Vorticity around Y for SOLID with ALE material law.
VORTZ
Vorticity around Z for SOLID with ALE material law.
VORT
Vorticity around for SOLID with ALE material law.
VOLU
Volume of each phase.
WPLA
Plastic work for /MAT/LAW12 (3D_COMP) and /MAT/LAW25 (COMPSH)
 

Comments

  1. For brick elements, the stresses are output in the elemental (corotational) coordinate system for /PROP/TYPE14 (SOLID) elements, and in the orthotropic material coordinate system for /PROP/TYPE6 (SOL_ORTH) elements if corotational formulation is used. For all other cases the stresses are output in the global coordinate system.
  2. Using /ANIM/BRICK/ORTHDIR with properties 6, 21, and 22 will output 3 real values of angle ψ , θ , and ϕ in unit [deg]. Defining rotation matrix R , to go from global reference system to orthotropic reference system:
    • Rotation matrices
    • A rotation of ψ radians about the x-axis is defined as:(1)
      R x ( ψ ) = [ 1 0 0 0 cos ψ sin ψ 0 sin ψ cos ψ ]
    • Similarly, a rotation of θ radians about the y-axis is defined as:(2)
      R y ( θ ) = [ cos θ 0 sin θ 0 1 0 sin θ 0 cos θ ]
    • Finally, a rotation of ϕ radians about the z-axis is defined as:(3)
      R z ( ϕ ) = [ cos ϕ sin ϕ 0 sin ϕ cos ϕ 0 0 0 1 ]
    • The angles ψ , θ , and ϕ are the Euler angles:(4)
      R = R z ( ϕ ) R y ( θ ) R x ( ψ )
      (5)
      R = [ cos θ cos ϕ sin ψ sin θ cos ϕ cos ψ sin ϕ cos ψ sin θ cos ϕ + sin ψ sin ϕ cos θ sin ϕ sin ψ sin θ sin ϕ + cos ψ cos ϕ cos ψ sin θ sin ϕ sin ψ cos ϕ sin θ sin ψ cos θ cos ψ cos θ ]
  3. The option SIGEQ is available with Eltyp = SHELL or BRICK only (/ANIM/SHELL/SIGEQ). Each material law, in Radioss has its own yield criterion to calculate the equivalent stress. For some it is von Mises; for others, it is Hill or Barlat or something else. For any non-von Mises criterion, the corresponded equivalent stress (or criterion) is computed within all the integration points of the element. Therefore, the output field /ANIM/BRICK/SIGEQ is computed as a mean value over all integration points.
  4. For brick elements, the stresses are output in the elemental (corotational) coordinate system for /PROP/SOLID elements, and in the orthotropic material coordinate system for /PROP/SOL_ORTH elements, when corotational formulation is used. For all other cases the stresses are output in the global coordinate system.
  5. The option /ANIM/ELEM/SIGX is only applied for shell elements. For brick elements, /ANIM/BRICK/TENS must be used.
  6. User variables are only available for shell and brick elements. When an integration point is not explicitly described, returned integration point means the integration point is superior; computed as [(number of integration points in thickness + 1) / 2]. The result is then rounded up to the superior value.
    • Example:

      For two integration points in thickness, second integration point from bottom (top of thickness) is returned.

      For three integration points in thickness, second integration point from bottom (middle one) is returned.

      For four integration points in thickness, third integration point from bottom is returned.

  7. The Schlieren contour value is computed using ξ = e c ρ MathType@MTEF@5@5@+= feaagKart1ev2aqatCvAUfeBSjuyZL2yd9gzLbvyNv2CaerbuLwBLn hiov2DGi1BTfMBaeXatLxBI9gBaerbd9wDYLwzYbItLDharqqtubsr 4rNCHbGeaGqiVu0Je9sqqrpepC0xbbL8F4rqqrFfpeea0xe9Lq=Jc9 vqaqpepm0xbba9pwe9Q8fs0=yqaqpepae9pg0FirpepeKkFr0xfr=x fr=xb9adbaqaaeGaciGaaiaabeqaamaabaabaaGcbaGaeqOVdGNaey ypa0JaamyzamaaCaaaleqabaGaeyOeI0Iaam4yaiabgEGirlabeg8a Ybaaaaa@3EF2@ . Radioss outputs ξ using c=1. The constant c MathType@MTEF@5@5@+= feaagKart1ev2aaatCvAUfeBSjuyZL2yd9gzLbvyNv2CaerbuLwBLn hiov2DGi1BTfMBaeXatLxBI9gBaerbd9wDYLwzYbItLDharqqtubsr 4rNCHbGeaGqiVu0Je9sqqrpepC0xbbL8F4rqqrFfpeea0xe9Lq=Jc9 vqaqpepm0xbba9pwe9Q8fs0=yqaqpepae9pg0FirpepeKkFr0xfr=x fr=xb9adbaqaaeGaciGaaiaabeqaamaabaabaaGcbaGaam4yaaaa@36DE@ can be updated using HyperView by creating a derived result ξ c u s e r MathType@MTEF@5@5@+= feaagKart1ev2aqatCvAUfeBSjuyZL2yd9gzLbvyNv2CaerbuLwBLn hiov2DGi1BTfMBaeXatLxBI9gBaerbd9wDYLwzYbItLDharqqtubsr 4rNCHbGeaGqiVu0Je9sqqrpepC0xbbL8F4rqqrFfpeea0xe9Lq=Jc9 vqaqpepm0xbba9pwe9Q8fs0=yqaqpepae9pg0FirpepeKkFr0xfr=x fr=xb9adbaqaaeGaciGaaiaabeqaamaabaabaaGcbaGaeqOVdG3aaW baaSqabeaacaWGJbWaaSbaaWqaaiaadwhacaWGZbGaamyzaiaadkha aeqaaaaaaaa@3CCF@ .
  8. For solid elements using LAW51, it is possible to display results for a given sub-material number (1 to 4) using:
    • /ANIM/ELEM/LAW51/ALL: results for all sub-material, or
      • /ANIM/ELEM/LAW51/1: results for sub-material 1
      • /ANIM/ELEM/LAW51/2: results for sub-material 2
      • /ANIM/ELEM/LAW51/3: results for sub-material 3
      • /ANIM/ELEM/LAW51/4: results for sub-material 4
      In this case, the following options can be displayed per phase:
      • /ANIM/ELEM/P
      • /ANIM/ELEM/DENS
      • /ANIM/ELEM/ENER
      • /ANIM/ELEM/SSP
      • /ANIM/ELEM/EPSP
      • /ANIM/ELEM/TEMP
      • /ANIM/ELEM/VOLU
      • /ANIM/MASS
  9. For quad or brick elements, /ANIM/ELEM/DAM1, /DAM2, and /DAM3 are available for material LAW24. These values are the principal values of the damage (values in the local cracking skew).
  10. Element time step is displayed in the animation only if elementary time step is computed for this element by Radioss. If nodal time step used (/DT/NODA) in the calculation, element time step is not displayed in the animation.
  11. Option DAMG is only used with coupled damage models (/MAT/LAW72 or /FAIL/GURSON) to output damage over integration points. The damage variable is normalized by its critical value.
    • For /MAT/LAW72(6)
      D m g = D D C MathType@MTEF@5@5@+= feaahqart1ev3aqatCvAUfeBSjuyZL2yd9gzLbvyNv2CaerbuLwBLn hiov2DGi1BTfMBaeXatLxBI9gBaerbd9wDYLwzYbItLDharqqtubsr 4rNCHbGeaGqiVCI8FfYJH8YrFfeuY=Hhbbf9v8qqaqFr0xc9pk0xbb a9q8WqFfeaY=biLkVcLq=JHqpepeea0=as0Fb9pgeaYRXxe9vr0=vr 0=vqpWqaaeaabiGaciaacaqabeaadaqaaqaaaOqaaabaaaaaaaaape GaamiramaaBaaaleaacaWGTbGaam4zaaqabaGccqGH9aqpdaWcaaWd aeaapeGaamiraaWdaeaapeGaamiramaaBaaaleaacaWGdbaabeaaaa aaaa@3CC0@
    • For /FAIL/GURSON(7)
      D m g = f t f F MathType@MTEF@5@5@+= feaahqart1ev3aqatCvAUfeBSjuyZL2yd9gzLbvyNv2CaerbuLwBLn hiov2DGi1BTfMBaeXatLxBI9gBaerbd9wDYLwzYbItLDharqqtubsr 4rNCHbGeaGqiVCI8FfYJH8YrFfeuY=Hhbbf9v8qqaqFr0xc9pk0xbb a9q8WqFfeaY=biLkVcLq=JHqpepeea0=as0Fb9pgeaYRXxe9vr0=vr 0=vqpWqaaeaabiGaciaacaqabeaadaqaaqaaaOqaaabaaaaaaaaape GaamiramaaBaaaleaacaWGTbGaam4zaaqabaGccqGH9aqpdaWcaaWd aeaapeGaamOza8aadaWgaaWcbaWdbiaadshaa8aabeaaaOqaa8qaca WGMbWdamaaBaaaleaapeGaamOraaWdaeqaaaaaaaa@3E83@
  12. If /NONLOCAL/MAT option is activated, it is possible to output the regularized non-local plastic strain and its rate.