I am going through the Formula 1 workshop and I have a question.
Session 2 covered a thermal stress analysis. In this session the exhaust was modeled and the stress was calculated using simple conduction and convection boundary conditions. In session 3 a CFD analysis is performed and the temperatures and pressures are calculated based on the airflow.
Is it possible to use the results of the CFD analysis (pressure and temperature) and apply these as boundary conditions in a structural analysis to calculate the stress and deformation of the exhaust?