/ANIM/BRICK/DAMA

Engine Keyword Generates animation files containing damage value as function of a solid element integration point. The damage value is the maximum of damage over time and of all failure criteria acting in one material.

Format

/ANIM/BRICK/DAMA/Keyword4

Definitions

Field Contents SI Unit Example
Keyword4 Integration Point Number:
0 or blank
Maximum integration point value in the element is output.
i, j, k
Value in integration Point of brick element.
i
Integration point number in direction r.
j
Integration point number in direction s.
k
Integration point number in direction t.
 

Comments

  1. If the integration point ijk does not exist in a solid, damage value is set to 0.
  2. If j is greater than or equal to 10 (in case of /PROP/TYPE22 (TSH_COMP)), syntax becomes:
    • /ANIM/BRICK/DAMA/i0k/j
    • With 10 ≤ j ≤ 200
  3. The damage value, D is 0 ≤ D ≤ 1. The status for fracture is:
    • Damage occurs, if 0 ≤ D < 1
    • Failure, if D = 1
  4. D is computed for every failure criteria as follows:
    • Strain-based failure (/FAIL/BIQUAD):(1)
      D = Δ ε p ε f
    • Johnson-Cook failure (/FAIL/JOHNSON): (2)
      D = Δ ɛ p ɛ f
    • Cockcroft Latham failure (/FAIL/COCKCROFT):(3)
      D = max ( σ 1 , 0 ) Δ ε p C 0 MathType@MTEF@5@5@+= feaagKart1ev2aqatCvAUfeBSjuyZL2yd9gzLbvyNv2CaerbuLwBLn hiov2DGi1BTfMBaeXatLxBI9gBaerbd9wDYLwzYbItLDharqqtubsr 4rNCHbGeaGqiVu0Je9sqqrpepC0xbbL8F4rqqrFfpeea0xe9Lq=Jc9 vqaqpepm0xbba9pwe9Q8fs0=yqaqpepae9pg0FirpepeKkFr0xfr=x fr=xb9adbaqaaeGaciGaaiaabeqaamaabaabaaGcbaGaamiraiabg2 da9maalaaabaWaaabqaeaaciGGTbGaaiyyaiaacIhacaGGOaGaeq4W dm3aaSbaaSqaaiaaigdaaeqaaOGaaiilaiaaicdacaGGPaGaeyyXIC TaeuiLdqKaeqyTdu2aaSbaaSqaaiaadchaaeqaaaqabeqaniabggHi LdaakeaacaWGdbGaaGimaaaaaaa@4A2E@
    • Tuler-Butcher failure (/FAIL/TBUTCHER): (4)
      D = 0 t ( σ σ r ) λ d t K
    • Wilkins failure (/FAIL/WILKINS): (5)
      D = W 1 W 2 d ε ¯ p D f
    • BAO-XUE-Wierzbicki failure (/FAIL/WIERZBICKI): (6)
      D = Δ ε p ε ¯ f
    • Strain failure model (/FAIL/TENSSTRAIN): (7)
      D = Max time ( ɛ 1 ɛ t 1 ɛ t 2 ɛ t 1 )
    • Energy density failure model (/FAIL/ENERGY): (8)
      D = M a x t i m e ( E E 1 E 2 E 1 )
    • Hashin Composite failure (/FAIL/HASHIN) - the maximum damage for different failure mode:
      • for uni-directional lamina mode(9)
        D = M a x ( F 1 , F 2 , F 3 , F 4 , F 5 ) MathType@MTEF@5@5@+= feaagKart1ev2aaatCvAUfeBSjuyZL2yd9gzLbvyNv2CaerbuLwBLn hiov2DGi1BTfMBaeXatLxBI9gBaerbd9wDYLwzYbItLDharqqtubsr 4rNCHbGeaGqiVu0Je9sqqrpepC0xbbL8F4rqqrFfpeea0xe9Lq=Jc9 vqaqpepm0xbba9pwe9Q8fs0=yqaqpepae9pg0FirpepeKkFr0xfr=x fr=xb9adbaqaaeGaciGaaiaabeqaamaabaabaaGcbaGaamiraiabg2 da9iaad2eacaWGHbGaamiEamaabmaabaGaamOramaaBaaaleaacaaI XaaabeaakiaacYcacaWGgbWaaSbaaSqaaiaaikdaaeqaaOGaaiilai aadAeadaWgaaWcbaGaaG4maaqabaGccaGGSaGaamOramaaBaaaleaa caaI0aaabeaakiaacYcacaWGgbWaaSbaaSqaaiaaiwdaaeqaaaGcca GLOaGaayzkaaaaaa@4779@
      • for fabric lamina model(10)
        D = M a x ( F 1 , F 2 , F 3 , F 4 , F 5 , F 6 , F 7 ) MathType@MTEF@5@5@+= feaagKart1ev2aaatCvAUfeBSjuyZL2yd9gzLbvyNv2CaerbuLwBLn hiov2DGi1BTfMBaeXatLxBI9gBaerbd9wDYLwzYbItLDharqqtubsr 4rNCHbGeaGqiVu0Je9sqqrpepC0xbbL8F4rqqrFfpeea0xe9Lq=Jc9 vqaqpepm0xbba9pwe9Q8fs0=yqaqpepae9pg0FirpepeKkFr0xfr=x fr=xb9adbaqaaeGaciGaaiaabeqaamaabaabaaGcbaGaamiraiabg2 da9iaad2eacaWGHbGaamiEamaabmaabaGaamOramaaBaaaleaacaaI XaaabeaakiaacYcacaWGgbWaaSbaaSqaaiaaikdaaeqaaOGaaiilai aadAeadaWgaaWcbaGaaG4maaqabaGccaGGSaGaamOramaaBaaaleaa caaI0aaabeaakiaacYcacaWGgbWaaSbaaSqaaiaaiwdaaeqaaOGaai ilaiaadAeadaWgaaWcbaGaaGOnaaqabaGccaGGSaGaamOramaaBaaa leaacaaI3aaabeaaaOGaayjkaiaawMcaaaaa@4C5C@
    • Puck Composite failure (/FAIL/PUCK) - the maximum damage for different failure mode: (11)
      D = Max ( e f ( tensile ) , e f ( compression ) , e f ( ModeA ) , e f ( ModeB ) , e f ( ModeC ) )
    • Ladeveze failure (/FAIL/LAD_DAMA)(12)
      d ˙ = k a [ 1exp( a w( Y )d ) ] MathType@MTEF@5@5@+= feaagKart1ev2aqatCvAUfeBSjuyZL2yd9gzLbvyNv2CaerbuLwBLn hiov2DGi1BTfMBaeXatLxBI9gBaerbd9wDYLwzYbItLDharqqtubsr 4rNCHbGeaGqiVu0Je9sqqrpepC0xbbL8F4rqqrFfpeea0xe9Lq=Jc9 vqaqpepm0xbba9pwe9Q8fs0=yqaqpepae9pg0FirpepeKkFr0xfr=x fr=xb9adbaqaaeGaciGaaiaabeqaamaabaabaaGcbaGabmizayaaca Gaeyypa0ZaaSaaaeaacaWGRbaabaGaamyyaaaadaWadaqaaiaaigda cqGHsislciGGLbGaaiiEaiaacchadaqadaqaaiabgkHiTiaadggada aadaqaaiaadEhadaqadaqaaiaadMfaaiaawIcacaGLPaaacqGHsisl caWGKbaacaGLPmIaayPkJaaacaGLOaGaayzkaaaacaGLBbGaayzxaa aaaa@4AAF@
    • Strain Failure Model with dependence on Lode angle (/FAIL/TAB1) (13)
      D = Δ D D c r i t
    • Spalling and Johnson-Cook failure (/FAIL/SPALLING): (14)
      D = Δ ɛ p ɛ ¯ f
    • Ladveze composite failure (/FAIL/LAD_DAMA): (15)
      D = k a [ 1 e ( a w ( Y ) d ) ]
    • Failure According (Normal and Tangential) Displacement Criteria and/or Energy Criteria (/FAIL/CONNECT): (16)
      D = Max time ( D max T max )
    • Failure According Plastic Displacement Criteria (/FAIL/SNCONNECT): (17)
      D = Max time ( u ¯ pl u ¯ 0 pl u ¯ f pl u ¯ 0 pl )
    • Extended Mohr Coulomb failure model (/FAIL/EMC):(18)
      D = M a x t i m e ( Δ ε ¯ p ε ¯ p , f a i l )