1. Reference problem#

1.1. Geometry#

_images/1000052400001B980000129BB7A905A498F51911.svg

1.2. Material properties#

The material obeys a law of behavior in large plastic deformations with linear isotropic work hardening, whose characteristics depend on temperature.

The tensile curve is given in the plane logarithmic deformation - rational stress.

_images/Object_1.svg
_images/10000BA4000069D500004B3E0227F64FC3AA1029.svg _images/Object_2.svg
_images/Object_3.svg

and

_images/Object_4.svg

are, respectively, the initial length and the current length of the useful part of the test piece.

_images/Object_5.svg

and

_images/Object_6.svg

are, respectively, the initial and current surfaces. Between temperatures \(20°C\) and \(120°C\), the characteristics are interpolated linearly.

1.3. Boundary conditions and loads#

The bar, of initial length

_images/Object_7.svg

, stuck in the direction

_images/Object_8.svg

on the side [1,2] is subjected to a uniform temperature

_images/Object_9.svg

and to a mechanical traction movement

_images/Object_10.svg

on side \(\mathrm{[}\mathrm{3,}4\mathrm{]}\). The loading sequences are as follows:

_images/10000DDE00000E2900000B440A7CDEAB66C949B6.svg _images/10000E8A00002D7A00000D3BC61E35BAFDB27AA4.svg

Reference temperature:

_images/Object_11.svg

=20°C.

Note:

The mechanical displacement is measured from the configuration deformed by thermal loading ( \(t\mathrm{=}\mathrm{1s}\) ). To get the total displacement, you must therefore add the thermal displacement obtained to the time \(t\mathrm{=}\mathrm{1s}\) .