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Gusts affect aircraft by increasing the aerodynamic loads applied to the structure. The mini-tab is proposed and evaluated as a potential control device to mitigate these increased aerodynamic loads.

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This page is a summary of: Dynamic Deployment of a Minitab for Aerodynamic Load Control, Journal of Aircraft, January 2020, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c035556.
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