Explicit dynamic

*Explicit Dynamic

*Explicit Dynamic
<Delta t_0>, <t_step>, [<Delta t_min>], [<Delta t_max>]
[*Mass Scaling=<>]

This procedure is used to calculate the response of a structure subject to dynamic loading using an explicit integration procedure of the equations of motion. In a dynamic step, loads are by default applied by their full magnitude at the start of the step. Other loading patterns can be prescribed by using previously defined amplitudes.

• The first line specifies the time incrementation. The specification of an initial time increment \(\Delta t_0\) is always required. \(t_{step}\) is the overall step time, which has to be specified in any case as well.\(\Delta t_{min}\) is the minimum used time increment, which may be omitted, and \(\Delta t_{max}\) is the maximum allowed time increment, which may be omitted as well. If only \(\Delta t_0\) and \(t_{step}\) are specified, the minimum stable time increment \(\Delta t_{crit}\) is used for all increments after the first increment. If \(\Delta t_{min}\) is given (and not equivalent to zero) \(\Delta t=\)\(\Delta t_{min}\) holds if \(\Delta t_{crit}<\)\(\Delta t_{min}\) . If \(\Delta t_{max}\) is given (\(\Delta t_{min}\) has to be defined in this case, potentially set to zero) \(\Delta t =\)\(\Delta t_{max}\) holds if \(\Delta t_{crit}>\)\(\Delta t_{max}\) . The value of \(\Delta t_{crit}\) can be scaled using the optional scale factor =< > as explained in the step definition.

• [*Mass Scaling=<>]
  

  Use this keyword to globally scale the mass by the specified factor, thereby increasing the minimum stable time increment \(\Delta t_{crit}\).

The following elements are supported in explicit analyses:

Element label	Dim	Shape	Nodes	Interpolation Order	nIP	Remarks
u4-solid-red	2D	rectangle	4	linear	1	(2)
u8-solid-3D-red	3D	brick	8	linear	1	(2)
u4u4-red	2D	rectangle	4	linear	1	(2)
u8u8-3d-red	3D	brick	8	linear	1	(2)

* nIP = number of integration points

(2) Reduced integration: This element does not suffer from the same locking issues as fully integrated elements, however, due to the rank deficiency of the element stiffness matrix, an Hourglass stiffness has to be applied to prevent spurious zero-energy modes. For more information see the *Material Section and the Theory Manual