.. _V7.01.100:

**v7.01.100** HPLA100 - Thermoelastic hollow cylinder weighing in uniform rotation
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**Summary**

The purpose of this test is to test the corresponding second members to the effects of gravity, thermal expansion and acceleration due to uniform rotation. For models :math:`C` and :math:`D` (shell :math:`\mathrm{3D}`), a chained thermo-elastic calculation and a thermoelastoplastic calculation without plastic evolution were carried out.

The results for the models are presented:


* :math:`\mathrm{2D}` axisymmetric: axisymmetric isoparametric finite elements on QUAD8 meshes,


* axisymmetric shells: axisymmetric isoparametric finite elements on SEG3 cells (linear mesh of the meridian section),


* shells :math:`\mathrm{3D}`: finite elements MEC3QU9H, MEC3TR7H on meshes QUAD9 and TRIA7, respectively,


* plates :math:`\mathrm{DKT}`: plane finite elements DKQ, DKT on meshes QUAD4 and TRIA3, respectively. We also test the orthotropic shells of DEFI_COMPOSITE for two layers of the same isotropic material and the keyword ELAS_COQU of DEFI_MATERIAU for the assignment of characteristics of homogenized plates.


.. toctree::
    :hidden:

    self

.. toctree::
    :maxdepth: 2
    :numbered:

    Probl_me_de_r_f_rence
    Solution_de_r_f_rence
    Mod_lisation_A
    Mod_lisation_B
    Mod_lisation_C
    Mod_lisation_D
    Mod_lisation_E
    Mod_lisation_F
    Mod_lisation_G

    Mod_lisation_H
    Mod_lisation_I
    Mod_lisation_J
    Mod_lisation_K
    Synth_se_des_r_sultats
    Annexe