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The dynamic behavior of beam-type structures, like helicopter or turbine pales, is substantially affected by their rotation angular velocity. Using a simple but detailed mathematical formulation, this paper discusses why and how this phenomenon occurs.

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This page is a summary of: Dynamics of Beams Undergoing Large Rotations Accounting for Arbitrary Axial Deformation, Journal of Guidance Control and Dynamics, July 2002, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/2.4957.
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