I want to assess the effect of high temperature property degradation on mechanical load in a multi component beam model. I have Tinit at a high temperature , 1300F, and Tload at a slightly higher 1301F. This is to place the components at a high temperature state with minimal thermal load generated. I Run a nastran deck with Tinit above the subcases, subcase 1 with mechanical load sufficient to yield some of the components which are at a high temperature. Subcase 2 with the thermal load. Then size HyperFEA. All components size to the room temperature allowable of IN718, though several components are overstressed at their actual Tinit, Tload temperature. Does HyperSizer account for material property degradation for components individually?
In 718 is temperature dependent with about a 50% reduction in Fty RT to 1300F.