Computational Nonlinear Aeroelasticity for Multidisciplinary Analysis and Design
Dr. Ramana Grandhi
Sponsors: AFRL, DAGSI, ITRI

One of the key elements in building airframes is developing materials that provide the needed structural integrity. This research focuses on dealing with the problem of airframe integrity by optimizing structural design. The goal is to maximize performance while minimizing weight. This research specifically looks at hypersonic vehicle design using multi-physics modeling of flow-behavior with high fidelity simulations. It integrates aerodynamics, structures, and controls with reduced-order systems for computationally efficient preliminary designs.

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