Active flutter control of thin walled wing-engine system using piezoelectric actuators
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DOI: 10.1016/j.ast.2020.105853
Abstract: Abstract In the present study, control of a Thin Walled Beam (TWB) wing-engine system is examined applying piezoelectric actuators to enhance the performance of aeroelastic response. The composite piezoelectric governing equations of motion including the… read more here.
Keywords: flutter; control; wing engine; engine system ... See more keywords