Inertia

class ansys.mapdl.core._commands.solution.inertia.Inertia

Inertia.acel([acel_x, acel_y, acel_z])	Specifies the linear acceleration of the global Cartesian reference frame for the analysis.
Inertia.airl([nrb, rigid_calc])	Specifies that automatic inertia relief calculations are to be performed.
Inertia.cgloc([xloc, yloc, zloc])	Specifies the origin location of the acceleration coordinate system.
Inertia.cgomga([cgomx, cgomy, cgomz])	Specifies the rotational velocity of the global origin.
Inertia.cmacel([cm_name, cmacel_x, ...])	Specifies the translational acceleration of an element component
Inertia.cmdomega([cm_name, domegax, ...])	Specifies the rotational acceleration of an element component about a user-defined rotational axis.
Inertia.cmomega([cm_name, omegax, omegay, ...])	Specifies the rotational velocity of an element component about a user-defined rotational axis.
Inertia.cmrotate([cm_name, rotatx, rotaty, ...])	Specifies the rotational velocity of an element component in a brake-squeal analysis.
Inertia.coriolis([option, refframe, ...])	Applies the Coriolis effect to a rotating structure.
Inertia.dcgomg([dcgox, dcgoy, dcgoz])	Specifies the rotational acceleration of the global origin.
Inertia.domega([domgx, domgy, domgz])	Specifies the rotational acceleration of the structure.
Inertia.irlf([key, printfreq, rampkey])	Specifies that inertia relief calculations are to be performed.
Inertia.omega([omegx, omegy, omegz])	Specifies the rotational velocity of the structure.
Inertia.synchro([ratio, cname])	Specifies whether the excitation frequency is synchronous or asynchronous with the rotational velocity of a structure.