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The Design and Operation of a Simple Low-Speed Flutter-Suppression Model.
AERONAUTICAL RESEARCH LABS MELBOURNE (AUSTRALIA)
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This Australian report discusses a dynamic model which has been developed for use in a small low-speed wind tunnel. A feedback system has been used to drive a control surface in order to suppress flutter. Details of the model and results of preliminary tests are presented. Keywords include Wind tunnel models, and Active Control.
APPROVED FOR PUBLIC RELEASE