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We discuss how wind tunnel model support system dynamics can limit the applicability of a force transducers static sensitivity. Tools are presented to help predict and avoid the limitations if possible. Finally, dynamic compensation strategies are discussed if the model support system dynamics cannot be avoided.

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This page is a summary of: Aerodynamic Metrologists Guide to Dynamic Force Measurement, Journal of Aircraft, June 2022, American Institute of Aeronautics and Astronautics (AIAA),
DOI: 10.2514/1.c036676.
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