1. Reference problem#
1.1. Geometry#
Coordinates of points \((m)\):
\(A:(0.,0.)\)
\(B:(1.,0.)\)
\(C:(1.,1.)\)
\(D:(0.\mathrm{,1}\mathrm{.})\)
1.2. Material properties#
Mechanics
\(E=1.N/{m}^{2}\)
\(\nu =0.\)
\(\alpha =1.°{C}^{-1}\)
Thermal
\(\lambda =1.w/m/°C\)
\(\rho \mathit{cp}\mathrm{=}1.J\mathrm{/}{m}^{3}°C\)
1.3. Boundary conditions and loads#
Compulsory trips:
\(A\): \(\mathrm{DX}=\mathrm{DY}=0.\)
\(B\): \(\mathrm{DY}=0.\)
Imposed thermal load:
Two homogeneous thermal evolutions in space are defined:
\(\mathrm{ch1}\) is a rise in temperature from 10 degrees to 17 degrees \([0.,0.7s]\)
\(\mathrm{ch2}\) is a drop in temperature from 17 degrees to 14 degrees \([0.,0.3s]\)
Cycle \([\mathrm{ch1}+\mathrm{ch2}]\) is staggered to form the interval \([1.5,2.5s]\). This cycle is repeated periodically and the mechanical calculation is performed over the interval \([0.5,4.5s]\).