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Thermoelastic Analysis with Blade Stiffened Shell Constitutive Model #314

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sean-engelstad
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Need: Perform aerostructural optimization in FUNtoFEM with TACSBladeStiffenedShellConstitutive constitutive model and Quad4ThermalShell elements.

  • Add thermal subroutines into TACSBladeStiffenedShellConstitutive class.
  • Add unittest for the constitutive model for a Quad4ThermalShell aka a thermoelastic shell

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