Reference problem ===================== Geometry --------- The structure is composed of a rotor of length :math:`L` with a variable circular section with two infinitely rigid bearings at the level of the supports. The diameters of the rotor section vary linearly depending on the length. Material properties ---------------------- The geometric and material characteristics are listed in the following table. +----------------+-------------------------------------------------------------------------+-----------------------------+-------------------------------------+----------------+ |Material |:math:`E=2{10}^{11}N/{m}^{2}`|:math:`\rho =7800\mathrm{kg}/{m}^{3}`|:math:`\nu =0.3`| +----------------+-------------------------------------------------------------------------+-----------------------------+-------------------------------------+----------------+ |Rotor length |:math:`L=1m` | +----------------+-------------------------------------------------------------------------+-----------------------------+-------------------------------------+----------------+ |Section diameter|original outer diameter: :math:`\mathrm{De1}=\mathrm{0,2}m` | + +-------------------------------------------------------------------------+-----------------------------+-------------------------------------+----------------+ | |final outer diameter: :math:`\mathrm{De2}=\mathrm{0,1}m` | +----------------+-------------------------------------------------------------------------+-----------------------------+-------------------------------------+----------------+ |Thickness |at any point on the rotor: :math:`\mathrm{De}–\mathrm{Di}=\mathrm{0,04}m` | +----------------+-------------------------------------------------------------------------+-----------------------------+-------------------------------------+----------------+ **Table** 1.2-1 The translation coefficients of the stages are: :math:`\mathrm{Kxx}=\mathrm{Kyy}=1.0E+12{\mathrm{kg.s}}^{-2}` :math:`\mathrm{Kxy}=\mathrm{Kyx}=0.0\mathrm{kg.s}-2` :math:`\mathrm{Cxx}=\mathrm{Cyy}=\mathrm{Cxy}=\mathrm{Cyx}=0.0{\mathrm{kg.s}}^{-1}` The torsional coefficients of the bearings are: :math:`\mathrm{Krz}=\mathrm{Kry}=1.0E+12{\mathrm{kg.s}}^{-2}` :math:`\mathrm{Kxy}=\mathrm{Kyx}=0.0\mathrm{kg.s}-2` :math:`\mathrm{Crx}=\mathrm{Cry}=\mathrm{Cxy}=\mathrm{Cyx}=0.0{\mathrm{kg.s}}^{-1}` Boundary conditions ---------------------- The rotor is supported on two rigid bearings at both ends.