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Unsteady aerodynamic reduced-order models seek to match the predictive capability of full-order CFD simulations, but at a significantly reduced computational cost. We demonstrate for the first time how to develop unsteady aerodynamic reduced-order models for flexible flight vehicles, including the impact of fluid-structure interactions on maneuvering vehicle aerodynamics.
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This page is a summary of: Aeroelastic Indicial Response Reduced-Order Modeling for Flexible Flight Vehicles, Journal of Aircraft, May 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c035646.
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