Examples
========


Degrees of freedom imposed in mechanics
--------------------------------------


.. code-block:: text

    dog = AFFE_CHAR_CINE (MODELE = me,
MECA_IMPO =(
_F (TOUT = 'OUI', DRZ = 0. ),
_F (GROUP_NO = 'edge1', DX = 0., DY = 0., DZ = 0. ,
DRX = 0., DRY = 0.,)))

For this plate problem in plane :math:`\mathrm{XY}`, we block all the degrees of freedom of rotation around :math:`Z` and we embed the plate on its edge :math:`\mathrm{bord1}`.


Comparative use of kinematic and "ordinary" loads
-------------------------------------------------------------


Global orders
~~~~~~~~~~~~~~~~~~~


.. code-block:: text

    ch1 = AFFE_CHAR_THER (...)

    ch2 = AFFE_CHAR_CINE_F (TEMP_IMPO = _F (...))

    evoth = THER_LINEAIRE (...
EXCIT = (_F (CHARGE = ch1),
_F (CHARGE = ch2),)
...)

There is no difference.


"Step by step" calculation
~~~~~~~~~~~~~~~~~~~

**Ordinary expenses**


.. code-block:: text
 ch1 = AFFE_CHAR_MECA (...)
honey = CALC_MATR_ELEM (... OPTION = 'RIGI_MECA', CHARGE = ch1)
matas = ASSE_MATRICE (MATR_ELEM = mel...)
matas = FACTORISER (reuse = matas, MATR_ASSE = matas)
U = RESOUDRE (MATR = field, CHAM_NO = F)

**Kinematic loads**


.. code-block:: text
 ch1 = AFFE_CHAR_CINE (...)
honey = CALC_MATR_ELEM (... OPTION = 'RIGI_MECA')
matas = ASSE_MATRICE (MATR_ELEM = mel,..., CHAR_CINE = ch1)
matas = FACTORISER (reuse = matas, MATR_ASSE = matas,)
vcine = CALC_CHAR_CINE (..., CHAR_CINE = ch2),
U = RESOUDRE (MATR = field, CHAM_NO = F,
CHAM_CINE = vcine)

The terms induced by the kinematic loads are carried over to the second member, which requires the calculation of a field at the additional nodes vcine by the command CALC_CHAR_CINE [U4.61.03].