Reference problem ===================== Geometry --------- Straight beam of length :math:`L`, with direction vector :math:`(\mathrm{4,}\mathrm{3,}0)`. +----------------------------------------------------------------------------------------------------------------------------+-----------------------------------------------------------------------------------------------------------------------------+ | | | + .. image:: images/10000000000001DE00000098DC1BD62BB1B66370.png + .. image:: images/100000000000009B0000006E5FDFFE913280E971.png + | :width: 3.978in | :width: 1.2807in | + :height: 1.2602in + :height: 0.9075in + | | | + + + | | | +----------------------------------------------------------------------------------------------------------------------------+-----------------------------------------------------------------------------------------------------------------------------+ | |**Pipe section** | +----------------------------------------------------------------------------------------------------------------------------+-----------------------------------------------------------------------------------------------------------------------------+ Tubular section with outer radius :math:`a\mathrm{=}\mathrm{0.04m}`, inner radius :math:`b\mathrm{=}\mathrm{0.032m}`, inner radius, and thickness :math:`e\mathrm{=}0.008m`. Material properties ----------------------- The material used has elastic behavior. The material parameters take the following values: • Young's module :math:`E=2.{10}^{11}\mathrm{Pa}`, • Poisson's ratio :math:`\nu =0.3`, • Density :math:`\rho =7800\mathrm{kg}/{m}^{3}`, • Thermal expansion coefficient :math:`\alpha ={10}^{-5}`. Boundary conditions and loads ------------------------------------- • Embedding in :math:`O` • 6 basic loads at the :math:`B` end • in coordinate :math:`(x,y,z)` linked to the beam: .. csv-table:: ":math:`{F}_{x}\mathrm{=}{5.10}^{2}N` "," :math:`{M}_{x}\mathrm{=}{5.10}^{2}\mathit{Nm}`" ":math:`{F}_{y}\mathrm{=}{5.10}^{2}N` "," :math:`{M}_{y}\mathrm{=}{5.10}^{2}\mathit{Nm}`" ":math:`{F}_{z}\mathrm{=}{5.10}^{2}N` "," :math:`{M}_{z}\mathrm{=}{5.10}^{2}\mathit{Nm}`" • or, in the global frame of reference :math:`(X,Y,Z)`: • 1 traction load: :math:`{F}_{X}={4.10}^{2}N` and :math:`{F}_{Y}={3.10}^{2}N` • 2 sharp efforts: in the :math:`(\mathrm{oxy})` :math:`{F}_{X}=–3.102N` and :math:`{F}_{Y}={4.10}^{2}N` plan and in the :math:`(\mathrm{oyz})` :math:`{F}_{Z}={5.10}^{2}N` plan • 1 torsional moment: :math:`{M}_{X}={4.10}^{2}\mathrm{Nm}` and :math:`{M}_{Y}={3.10}^{2}\mathrm{Nm}` • 2 sharp efforts: in the :math:`(\mathrm{oxy})` :math:`{M}_{X}\mathrm{=}–{3.10}^{2}\mathit{Nm}` and :math:`{M}_{Y}\mathrm{=}{4.10}^{2}\mathit{Nm}` plan and in the :math:`(\mathrm{oyz})` :math:`{M}_{Z}\mathrm{=}{5.10}^{2}\mathit{Nm}` plan • Internal pressure: :math:`P={10}^{7}\mathrm{Pa}` • Gravity, with :math:`g=\mathrm{10m}/{s}^{2}`, in the :math:`-Z` direction • Line load, :math:`\mathrm{Fz}=-141.146N/m` (which corresponds to the load due to gravity: :math:`\mathrm{Fz}=\mathrm{mg}`) • Thermal expansion: :math:`\mathrm{Temp}=100°C` Notation of cross-sectional characteristics -------------------------------------------------------- The geometric characteristics of the cross sections are noted: • :math:`S`: area of the section • :math:`{I}_{y},{I}_{z}`: geometric moments of inertia in relation to the main axes of inertia of the section • :math:`{J}_{x}`: torsional constant