Design improvements and flap deflection evaluations with considering centrifugal load on active trailing edge flap
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DOI: 10.1108/aeat-10-2016-0165
Abstract: The purpose of this paper is to present the design, analysis and experiments of the active trailing-edge flap (Seoul National University Flap, SNUF) for vibration reduction in the helicopter rotor prior to the small-scale blades… read more here.
Keywords: active trailing; trailing edge; flap; analysis ... See more keywords