fedoo.constitutivelaw.ShellHomogeneous

class ShellHomogeneous(material, thickness, k=1, name='')

__init__(material, thickness, k=1, name='')

Methods

ShellHomogeneous.compute_area_density()
ShellHomogeneous.compute_rotary_density()
ShellHomogeneous.get_all()	Return a dict with all the known ConstitutiveLaw (with a name).
ShellHomogeneous.get_local_frame([assembly])	Return material frames, resolved at assembly Gauss points.
ShellHomogeneous.get_shell_stiffness_matrix()
ShellHomogeneous.get_strain(assembly, **kargs)	Return the last computed strain associated to the given assembly.
ShellHomogeneous.get_stress(assembly, **kargs)
ShellHomogeneous.get_stress_distribution(...)
ShellHomogeneous.initialize(assembly, pb)	Initialize the constitutive law for the current problem.
ShellHomogeneous.reset()	Reset the constitutive law.
ShellHomogeneous.set_local_frame(local_frame)	Define the material coordinate frame.
ShellHomogeneous.set_start(assembly, pb)	Begin a new time iteration.
ShellHomogeneous.to_start(assembly, pb)	Restart the current time iteration.
ShellHomogeneous.update(assembly, pb)	Update shell stress from the strain computed by the weak form.

ShellHomogeneous.area_density	Mass per unit midsurface area.
ShellHomogeneous.name	Name of the constitutive law.
ShellHomogeneous.rotary_density	Mass moment of inertia per unit midsurface area.
ShellHomogeneous.thickness	Shell thickness.
ShellHomogeneous.k	Shear shape factor.
ShellHomogeneous.is_initialized	Tag set to True once the law is intialized.