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It is common practice in many engineering applications to use simplified 2D modelling to estimate the loads acting on wings and rotor blades as a result of turbulence, or "gusts". However, this is not appropriate on geometries that are strongly three-dimensional. This study explores the limits of applicability of 2D modelling on 3D geometries, and demonstrates some of the fundamental differences between unsteady flow response in 2D and 3D.

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This page is a summary of: Effect of Three-Dimensional Geometry on Harmonic Gust–Airfoil Interaction, AIAA Journal, February 2021, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.j059661.
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