/HEAT/MAT

Block Format Keyword Describes thermal parameters for thermal analysis.

Format

(1) (2) (3) (4) (5) (6) (7) (8) (9) (10)
/HEAT/MAT/mat_ID/unit_ID
T0 ρ 0 C p AS BS Iform  
T1 AL BL EFRAC    

Definitions

Field Contents SI Unit Example
mat_ID Material identifier.

(Integer, maximum 10 digits)

 
unit_ID Unit Identifier.

(Integer, maximum 10 digits)

 
T0 Initial temperature (1st part).

Default = 300K (Real)

[ K ]
ρ 0 C p (Mandatory) Specific heat per unit volume.

(Real)

[ J m 3 K ]
AS Thermal conductivity coefficient A for solid phase.

(Real)

[ W m K ]
BS Thermal conductivity coefficient B for solid phase.

(Real)

[ W m K 2 ]
Iform Heat transfer formulation flag.
= 0 (Default)
For ALE formulation or /MAT/LAW18 (THERM), based on finite volume method, is available for ALE solid element.
= 1
For Lagrangian formulation, based on finite element method, is available for solid and shell elements.

(Integer)

 
T1 Temperature of melting point.

Default = 1020 (Real)

[ K ]
AL Thermal conductivity coefficient A for liquid phase.

(Real)

[ W m K ]
BL Thermal conductivity coefficient B for liquid phase.

(Real)

[ W m K 2 ]
EFRAC Fraction of strain energy converted into heat.

Default = 1. (Real)

 

Example (Thermal)

#RADIOSS STARTER
#---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----|
#-  1. MATERIALS:
#---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----|
/UNIT/1
unit for mat
                  Mg                  mm                   s
#---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----|
/MAT/PLAS_JOHNS/1/1
Steel 
#              RHO_I
              7.8E-9                   0
#                  E                  Nu
              210000                  .3
#                  a                   b                   n           EPS_p_max            SIG_max0
                 270                 450                  .6                   0                   0
#                  c           EPS_DOT_0       ICC   Fsmooth               F_cut               Chard
                   0                   0         0         0                   0                   0
#                  m              T_melt              rhoC_p                 T_r
                   0                   0                   0                   0
/HEAT/MAT/1/1
#                 T0             RHO0_CP                  AS                  BS     IFORM
                 273               3.588                19.0                   0         1
# Blank card

/THERM_STRESS/MAT/1/1
# func_IDT            Fscale_y
      1003                   0
#---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----|
#-  2. FUNCTIONS:
#---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----|
/FUNCT/1003
linear expansion coefficient funtion of temperature
#                  X                   Y
                 273              1.2E-5                                                            
                 800              1.2E-5                                                            
#---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----|
#enddata
#---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----|

Comments

  1. ρ 0 C p is a mandatory option; otherwise, Starter will error out.
  2. Values defined in this card overwrite the equivalent values defined in the material.
  3. This option is available for all material laws; except the following:

    LAW0, 5, 6, 11, 21, 26, 37, 41, 46, 51, 54, 97, 108, 113, 151, /MAT/B-K-EPS, /MAT/K-EPS, and /MAT/GAS

  4. This option is compatible with equations of state, /EOS, only when used with the following materials: LAW3, 4, 12, and 49
  5. This option is available for:
    • All shell elements formulations; except DKT18 and T6
    • All solid elements formulations; except PA6
  6. The k MathType@MTEF@5@5@+= feaagKart1ev2aaatCvAUfeBSjuyZL2yd9gzLbvyNv2CaerbwvMCKf MBHbqefqvATv2CG4uz3bIuV1wyUbqedmvETj2BSbqefm0B1jxALjhi ov2DaebbnrfifHhDYfgasaacH8srps0lbbf9q8WrFfeuY=Hhbbf9v8 qqaqFr0xc9pk0xbba9q8WqFfea0=yr0RYxir=Jbba9q8aq0=yq=He9 q8qqQ8frFve9Fve9Ff0dmeaacaGacmGadaWaaiqacaabaiaafaaake aacaWGRbaaaa@39C7@ (thermal conductivity) is computed as:(1)
    k = A S + B S * T MathType@MTEF@5@5@+= feaagKart1ev2aaatCvAUfeBSjuyZL2yd9gzLbvyNv2CaerbuLwBLn hiov2DGi1BTfMBaeXatLxBI9gBaerbd9wDYLwzYbItLDharqqtubsr 4rNCHbGeaGqiVu0Je9sqqrpepC0xbbL8F4rqqrFfpeea0xe9Lq=Jc9 vqaqpepm0xbba9pwe9Q8fs0=yqaqpepae9pg0FirpepeKkFr0xfr=x fr=xb9adbaqaaeGaciGaaiaabeqaamaabaabaaGcbaGaam4Aaiabg2 da9iaadgeacaWGtbGaey4kaSIaamOqaiaadofacaGGQaGaamivaaaa @3D92@

    Where, T MathType@MTEF@5@5@+= feaagKart1ev2aaatCvAUfeBSjuyZL2yd9gzLbvyNv2CaerbuLwBLn hiov2DGi1BTfMBaeXatLxBI9gBaerbd9wDYLwzYbItLDharqqtubsr 4rNCHbGeaGqiVu0Je9sqqrpepC0xbbL8F4rqqrFfpeea0xe9Lq=Jc9 vqaqpepm0xbba9pwe9Q8fs0=yqaqpepae9pg0FirpepeKkFr0xfr=x fr=xb9adbaqaaeGaciGaaiaabeqaamaabaabaaGcbaGaamivaaaa@36CF@ is the current temperature in Kelvin.

  7. The α (thermal diffusivity) is computed as:(2)
    α = k ρ 0 C p

    Where, C p MathType@MTEF@5@5@+= feaagKart1ev2aaatCvAUfeBSjuyZL2yd9gzLbvyNv2CaerbuLwBLn hiov2DGi1BTfMBaeXatLxBI9gBaerbd9wDYLwzYbItLDharqqtubsr 4rNCHbGeaGqiVu0Je9sqqrpepC0xbbL8F4rqqrFfpeea0xe9Lq=Jc9 vqaqpepm0xbba9pwe9Q8fs0=yqaqpepae9pg0FirpepeKkFr0xfr=x fr=xb9adbaqaaeGaciGaaiaabeqaamaabaabaaGcbaGaam4qamaaBa aaleaacaWGWbaabeaaaaa@37DF@ is the heat capacity at constant pressure.

  8. New k ' MathType@MTEF@5@5@+= feaagKart1ev2aaatCvAUfeBSjuyZL2yd9gzLbvyNv2CaerbwvMCKf MBHbqefqvATv2CG4uz3bIuV1wyUbqedmvETj2BSbqefm0B1jxALjhi ov2DaebbnrfifHhDYfgasaacH8srps0lbbf9q8WrFfeuY=Hhbbf9v8 qqaqFr0xc9pk0xbba9q8WqFfea0=yr0RYxir=Jbba9q8aq0=yq=He9 q8qqQ8frFve9Fve9Ff0dmeaacaGacmGadaWaaiqacaabaiaafaaake aacaWGRbGaai4jaaaa@3A72@ (thermal conductivity) is computed as:(3)
    k ' = A L + B L * T MathType@MTEF@5@5@+= feaagKart1ev2aaatCvAUfeBSjuyZL2yd9gzLbvyNv2CaerbuLwBLn hiov2DGi1BTfMBaeXatLxBI9gBaerbd9wDYLwzYbItLDharqqtubsr 4rNCHbGeaGqiVu0Je9sqqrpepC0xbbL8F4rqqrFfpeea0xe9Lq=Jc9 vqaqpepm0xbba9pwe9Q8fs0=yqaqpepae9pg0FirpepeKkFr0xfr=x fr=xb9adbaqaaeGaciGaaiaabeqaamaabaabaaGcbaGaam4AaiaacE cacqGH9aqpcaWGbbGaamitaiabgUcaRiaadkeacaWGmbGaaiOkaiaa dsfaaaa@3E2F@
  9. T1, AL, and BL can be used only for solid elements when finite volume method is used (Iform = 0).
  10. There is no thermal coupling between an ALE thermal material and a Lagrangian thermal material.