Air#

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:
namestr

Material name.

mass_densityfloat, optional

Mass density. The default is 0.00128.

pressure_cutofffloat, optional

pressure cutoff. The default is 1e-09.

initial_internal_energyfloat, optional

Initial internal energy per unit reference volume. The default is 2.5331e-06.

initial_relative_volumefloat, optional

Initial relative volume. The default is 1.0.

equation_coefficientlist, optional

Six polynomial equation coefficient. The default is [0, 0, 0, 0, 0.4, 0.4, 0]).

Returns:
bool

True when successful, False when failed.

Overview#

Import detail#

from ansys.dyna.core.pre.dynamaterial import Air

Attribute detail#

Air.mass_density = 0.00128#
Air.pressure_cutoff = -1e-09#
Air.initial_internal_energy = 2.5331e-06#
Air.initial_relative_volume = 1.0#
Air.equation_coefficient = [0, 0, 0, 0, 0.4, 0.4, 0]#

Method detail#

Air.create(stub)#

Create an air material.