Reduced-order thrust modeling for an efficiently flapping airfoil using system identification method
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DOI: 10.1016/j.jfluidstructs.2016.12.005
Abstract: Abstract This paper presents a novel reduced-order model (ROM) of thrust for an efficiently flapping airfoil using system identification method. A NACA0012 airfoil pitching and plunging at a low Reynolds number of 40,000 is used… read more here.
Keywords: reduced order; airfoil using; efficiently flapping; method ... See more keywords