Block Format Keyword
/MAT/LAW74 - Thermal Hill Orthotropic 3D Material
Description
This law describes the Thermal Hill orthotropic 3D material and is applicable only to solid elements. The yield stress may depend on strain rate, or on both strain rate and temperature.
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/MAT/LAW74/mat_ID/unit_ID |
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fct_IDE |
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Einf |
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Ti |
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#RADIOSS STARTER #---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----| /UNIT/1 unit for mat g mm ms #---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----| #- 2. MATERIALS: #---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----| /MAT/LAW74/1/1 Aluminum # RHO_I .0027 # E NU EPSILON_P_MAX EPSILON_T EPSILON_M 60400 .33 0 0 0 # fct_ID EINF CE 0 0 0 # FSMOOTH C_HARD FCUT 1 0 10 # SIGMA11Y SIGMA22Y SIGMA33Y 1 1 1 # SIGMA12Y SIGMA23Y SIGMA31Y 1 1 1 # TABLE SIGMA_SCALE EPSPT_SCALE 10 0 0 # TI RHO0_CP 0 0 #---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----| #- 3. FUNCTIONS: #---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----| /TABLE/1/10 table #DIMENSION 3 # fct_ID X Z 38 0 293 38 10 293 39 11 293 40 20 293 38 0 400 38 10 400 39 11 400 40 20 400 #---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----| /FUNCT/38 function_38 # X Y 0 90 2.5E-4 100 .001 104.5 .009 121 .01 136 .02 143.5 .04 163 .07 169.5 #---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----| /FUNCT/39 function_39 # X Y 0 108 2.5E-4 120 .001 125.4 .009 145.2 .01 163.2 .02 172.2 .04 195.6 .07 203.4 #---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----| /FUNCT/40 function_40 # X Y 0 126 2.5E-4 140 .001 146.3 .009 169.4 .01 190.4 .02 200.9 .04 228.2 .07 237.3 #---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----| #ENDDATA /END #---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----| |
Where, Where, and represent the stress components either in the orthotropic frame if an orthotropic property is used, or in the orthogonalized isoparametric frame.
If or falls out of the range of the table, yield stress is obtained by linear extrapolation. Thus it is necessary to input into the table the static curves corresponding to zero strain rate (entry should belong to the table definition). Values of the table are yield stress values.
If the /HEAT/MAT option is not associated to the material identifier, adiabatic conditions are assumed and temperature is computed as: where, Eint is the internal energy computed by RADIOSS, and Volume are the current density and volume, Cp is the heat capacity per mass unit. Otherwise, the finite element formulation for heat transfer must be asked for (Iform =1 in option /HEAT/MAT); initial temperature and specific heat input in the option /HEAT/MAT will then be used.
The initial value of the scale factor should be equal to 1 and it decreases.
Where, E and Einf are respectively the initial and asymptotic value of Young’s modulus, accumulated equivalent plastic strain. Note: If fct_IDE = 0 and CE = 0, Young modulus E is kept constant. |
See Also: