The Shape Memory Alloy feature is used to model stress-strain relationships which are nonlinear even at infinitesimal strains. It is available in the Solid Mechanics interface. This material model requires the Nonlinear Structural Materials Module.
By adding the following subnodes to the Shape Memory Alloy node you can incorporate other effects:
From the Temperature T list, select an existing temperature variable from a heat transfer interface (for example,
Temperature (ht)), if any temperature variables exist, or select
User defined to enter a value or expression for the temperature.
If any material in the model has a temperature dependent mass density, and From material is selected for the density, the
Volume reference temperature list will appear in the
Model Input section. As a default, the value of
Tref is obtained from a
Common model input. You can also select
User defined to enter a value or expression for the reference temperature locally.
When using Common model input, you can see or modify the value of the volume reference temperature by clicking the
Go To Source button (
). This will move you to the
Common Model Inputs node under
Global Definitions in the Model Builder. The default value is room temperature;
293.15 K.
If you want to create a model input value which is local to your current selection, click the Create Model Input button
. This will create a new
Model Input node under
Definitions in the current component, having the same selection as in the current node.
The Global coordinate system is selected by default. The
Coordinate system list contains any additional coordinate systems that the model includes (except boundary coordinate systems). The coordinate system is used when stresses or strains are presented in a local system. The coordinate system must have orthonormal coordinate axes, and be defined in the material frame. Many of the possible subnodes inherit the coordinate system settings.
For Lagoudas enter the
Shape memory alloy reference temperature T0. The defaults for the
Poisson’s ratio ν and
Density ρ, are taken
From material. For
User defined enter other values or expressions.
For Austenite, select a material from the list. The
Young’s modulus EA and the
Heat capacity at constant pressure Cp,A are taken from the selected material. For
Martensite, select a material from the list. The
Young’s modulus EM and the
Heat capacity at constant pressure Cp,M are taken from the selected material. For
User defined enter other values or expressions.
For Smooth, enter the smoothing parameters
η1,
η2,
η3, and
η4.
For Souza-Auriccio the defaults for the
Poisson’s ratio ν and
Density ρ, are taken
From material. For
User defined enter other values or expressions.
For Austenite, select a material from the list. The
Young’s modulus EA is taken from the selected material. For
Martensite, select a material from the list. The
Young’s modulus EM is taken from the selected material. For
User defined enter other values or expressions.
Select the Calculate dissipated energy check box as needed to compute the energy dissipated.