Abstract

The paper discusses current approaches for the use of computational fluid dynamics in aeroelastic analyses and structural design optimization applications. Current methods for computational fluid dynamics-based static maneuver load analysis and flutter analysis are reviewed, including related issues such as fluid-structure interface, and moving mesh. Present state-of-the-art examples from the literature are presented along with research studies by the author. The paper highlights the challenges of computational fluid dynamics-based aeroelastic methods and their incorporation into aircraft structural design.

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