workbench please reply the student community is a public forum for authorized ansys academic product users to share ideas and ask questions, ansys materials continued metallic linear low deflection room temperature plasticity large deflection permanent deformation temperature effect
The application and workflow of Computational Fluid Dynamics (CFD)/Computational Structure Dynamics (CSD) on solving the static aeroelastic problem of a slender rocket are introduced. To predict static aeroelastic behavior accurately, two-way coupling and inertia relief methods are used to calculate the static deformations and aerodynamic characteristics of the deformed rocket.