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A method for creating self-induced coupled roll and yaw oscillations for aircraft models in a wind tunnel is presented. The mechanism for this is derived mathematically and investigations on stability of the system and its sensitivity to testing parameters are discussed.
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This page is a summary of: Self-Induced Roll–Yaw Oscillations of an Aircraft Model in a Wind Tunnel, Journal of Aircraft, January 2022, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c036157.
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