ansys.dyna.core.pre.dynamaterial.Air ==================================== .. py:class:: ansys.dyna.core.pre.dynamaterial.Air(mass_density=0.00128, pressure_cutoff=-1e-09, initial_internal_energy=2.5331e-06, initial_relative_volume=1.0, equation_coefficient=[0, 0, 0, 0, 0.4, 0.4, 0]) Defines an air material. :Parameters: **name** : :class:`python:str` Material name. **mass_density** : :class:`python:float`, :obj:`optional` Mass density. The default is ``0.00128``. **pressure_cutoff** : :class:`python:float`, :obj:`optional` pressure cutoff. The default is ``1e-09``. **initial_internal_energy** : :class:`python:float`, :obj:`optional` Initial internal energy per unit reference volume. The default is ``2.5331e-06``. **initial_relative_volume** : :class:`python:float`, :obj:`optional` Initial relative volume. The default is ``1.0``. **equation_coefficient** : :class:`python:list`, :obj:`optional` Six polynomial equation coefficient. The default is ``[0, 0, 0, 0, 0.4, 0.4, 0])``. :Returns: :ref:`bool ` ``True`` when successful, ``False`` when failed. .. !! processed by numpydoc !! .. py:attribute:: mass_density :value: 0.00128 .. py:attribute:: pressure_cutoff :value: -1e-09 .. py:attribute:: initial_internal_energy :value: 2.5331e-06 .. py:attribute:: initial_relative_volume :value: 1.0 .. py:attribute:: equation_coefficient :value: [0, 0, 0, 0, 0.4, 0.4, 0] .. py:method:: create(stub) Create an air material. .. !! processed by numpydoc !!