/MAT/LAW71

Block Format Keyword This law describes the behavior of superelastic materials. It allows modeling the behavior of the shape memory alloys (such as Nitinol).

The particularity of these materials is that all of the strain is recovered upon unloading even when large deformations are reached. Besides, the material shows a hysteretic response in a complete loading-unloading cycle. The full recovery is due to phase change in the microstructure. The model is based on the work of Auricchio et al. 1997. This law is compatible with solid and shell elements.

Format

(1) (2) (3) (4) (5) (6) (7) (8) (9) (10)
/MAT/LAW71/mat_ID/unit_ID
mat_title
ρ i                
E υ E_mart        
σ sas σ fas σ ssa σ fsa α
EpsL CAS CSA TSAS TFAS
TSSA TFSA Cp Tini  

Definitions

Field Contents SI Unit Example
mat_ID Material identifier

(Integer, maximum 10 digits)

 
unit_ID Unit Identifier

(Integer, maximum 10 digits)

 
mat_title Material title

(Character, maximum 100 characters)

 
ρ i Initial density

(Real)

[ kg m 3 ]
E Young's modulus

(Real)

[ Pa ]
υ Poisson's ratio

(Real)

 
E_mart Martensite Young's modulus (only available for solid element).
0
E is austenite young's modulus.

Default = E

(Real)

[ Pa ]
σ sas Material parameter defining the start of phase transformation from austenite to martensite (AS). 1

(Real)

[ Pa ]
σ fas Material parameter defining the end of phase transformation from austenite to martensite (AS). 1

(Real)

[ Pa ]
σ ssa Material parameter defining the start of phase transformation from martensite to austenite (SA). 1

(Real)

[ Pa ]
σ fsa Material parameter defining the end of phase transformation from martensite to austenite (SA). 1

(Real)

[ Pa ]
α Material parameter measuring the difference in response between tension and compression.

Default = 0 (Real)

 
EpsL Maximum residual strain. 2

(Real)

 
CAS Stress-Temperature rate during loading.

Default = 0 (Real)

[ Pa K ]
CSA Stress-Temperature rate during unloading.

Default = 0 (Real)

[ Pa K ]
TSAS Initial temperature for transformation (AS).

Default = 0 (Real)

[ K ]
TFAS Final temperature for transformation (AS).

Default = 0 (Real)

[ K ]
TSSA Initial temperature for transformation (SA).

Default = 0 (Real)

[ K ]
TFSA Final temperature for transformation (SA).

Default = 0 (Real)

[ K ]
Cp Specific heat capacity.

Default = 1030 (Real)

[ J kgK ] MathType@MTEF@5@5@+= feaagKart1ev2aaatCvAUfeBSjuyZL2yd9gzLbvyNv2CaerbuLwBLn hiov2DGi1BTfMBaeXatLxBI9gBaerbd9wDYLwzYbItLDharqqtubsr 4rNCHbGeaGqiVu0Je9sqqrpepC0xbbL8F4rqqrFfpeea0xe9Lq=Jc9 vqaqpepm0xbba9pwe9Q8fs0=yqaqpepae9pg0FirpepeKkFr0xfr=x fr=xb9adbaqaaeaaciGaaiaabeqaamaabaabaaGcbaWaamWaaeaada WcaaqaaiaabQeaaeaacaqGRbGaae4zaiabgwSixlaabUeaaaaacaGL BbGaayzxaaaaaa@3DB3@
Tini Initial temperature.

Default = 360 K (Real)

[ K ]

Example

#RADIOSS STARTER
#---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----|
#-  2. MATERIALS:
#---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----|
/MAT/LAW71/1/1
metal
#              RHO_I
             6.50E-9
#                  E                  Nu              E_mart
               62500                  .3               51000
#            sig_sas             sig_fas             sig_ssa             sig_fsa               alpha
                 450                 600                 300                 200                0.20
#               EpsL                 CAS                 CSA                TSAS                TFAS
               0.045                   1                   1                 383                 343
#               TSSA                TFSA                  CP                TINI
                 363                 403                 837                 360
#ENDDATA
/END
#---1----|----2----|----3----|----4----|----5----|----6----|----7----|----8----|----9----|---10----|

Comments

  1. The different stresses defining the start and the end of phase transformations, as well as the residual strain, correspond to the case of a uniaxial tensile test.
  2. The parameter α is computed from the initial value of the A → S phase transformation in tension ( σ sas ) T and compression ( σ sas ) C from the relation:(1)
    α 2 3 ( σ sas ) C ( σ sas ) T ( σ sas ) C + ( σ sas ) T

    law71_transformation
    Figure 1.
    List of Animation output (/ANIM/BRICK/USRI):
    • USR 1= Martensite phase fraction
    • USR 2= Loading function
    • USR 3= Unloading function