fedoo.constitutivelaw.ShellLaminate

class ShellLaminate(listMat, list_thickness, k=1, name='')

__init__(listMat, list_thickness, k=1, name='')

Methods

ShellLaminate.GetStressDistribution(assembly, pg)
ShellLaminate.find_layer([position])	Return the id of layer at a given position in the thickness.
ShellLaminate.get_all()	Return a dict with all the known ConstitutiveLaw (with a name).
ShellLaminate.get_shell_stiffness_matrix()
ShellLaminate.get_shell_stiffness_matrix_FI()
ShellLaminate.get_shell_stiffness_matrix_RI()
ShellLaminate.get_strain(assembly, **kargs)	Return the last computed strain associated to the given assembly.
ShellLaminate.get_stress(assembly, **kargs)
ShellLaminate.initialize(assembly, pb)	Initialize the constitutive law for the current problem.
ShellLaminate.reset()	Reset the constitutive law.
ShellLaminate.set_start(assembly, pb)	Begin a new time iteration.
ShellLaminate.to_start(assembly, pb)	Restart the current time iteration.
ShellLaminate.update(assembly, pb)	Update the constitutive law for the current problem state.

ShellLaminate.name	Name of the constitutive law.
ShellLaminate.thickness	Shell thickness.
ShellLaminate.k	Shear shape factor.
ShellLaminate.is_initialized	Tag set to True once the law is intialized.