Fluid-Structure Interaction and Coupled Sensitivity Analysis for Design Optimization of Both Static and Dynamic Aeroelastic Problems
Dr. Seongim Choi, Aerospace and Ocean Engineering, VirginiaTech
High-fidelity analysis and design of dynamic aeroelasctic problems, including aircraft wing flutter or helicopter rotor blades flows in forward flight, requires time-dependent solutions of both aerodynamics and structures.
Contact: Megan Autry