Nitinol Material Property Definition
Description: Defines material properties for use in shape memory alloys (Nitinol).
Format:
Example:
Field | Definition | Type | Default |
---|---|---|---|
MID | Identification number of a MAT1 entry. | Integer > 0 | Required |
ALPHA | Pressure coefficient. | Real ≥ 0 | 0.1 |
ELMAX | Maximum residual strain. | Real ≥ 0 | 0.1 |
CAS | Conversion constant from austenite to martensite. | Real ≥ 0 | 1.0 |
CSA | Conversion constant from martensite to austenite. | Real ≥ 0 | 1.0 |
TSAS | Starting temperature of transformation from austenite to martensite. | Real | 0.0 See Remark 1 |
TFAS | Ending temperature of transformation from austenite to martensite. | Real | 0.0 See Remark 1 |
TSSA | Starting temperature of transformation from martensite to austenite. | Real | 0.0 See Remark 1 |
TFSA | Ending temperature of transformation from martensite to austenite. | Real | 0.0 See Remark 1 |
BTAS | Constant for exponential flow rule (austenite to martensite). | Real ≥ 0 | 0.0 See Remark 2 |
BTSA | Constant for exponential flow rule (martensite to austenite). | Real ≥ 0 | 0.0 See Remark 2 |
SSAS | Starting stress for transformation from austenite to martensite at reference temperature. | Real | 0.0 See Remark 3 |
SFAS | Ending stress for transformation from austenite to martensite at reference temperature. | Real | 0.0 See Remark 3 |
SSSA | Starting stress for transformation from martensite to austenite at reference temperature. | Real | 0.0 See Remark 3 |
SFSA | Ending stress for transformation from martensite to austenite at reference temperature. | Real | 0.0 See Remark 3 |
Remarks:
- The following relations must be satisfied between the four temperatures:
TFAS < TSAS < TSSA < TFSA
- When BTAS and BTSA are zero the material model is linear. When BTAS and BTSA are non-zero the material model is exponential with BTAS and BTSA as coefficients.
- The transformation stresses and temperature can be combined such that the transformation stress can be calculated by
- Starting stress for transformation from austenite to martensite = SSAS - CAS*TSAS
- Ending stress for transformation from austenite to martensite = SFAS - CAS*TFAS
- Starting stress for transformation from martensite to austenite = SSSA - CSA*TSSA
- Ending stress for transformation from martensite to austenite = SFSA - CSA*TFSA
Figure 1. Stress-Temperature Transformation Variables