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Published in 2017 at "AIAA Journal"
DOI: 10.2514/1.j055354
Abstract: The ability of vortex generators to reduce the unsteady distortion at the exit plane of an S duct is investigated. The three components of the velocity at the aerodynamic interface plane were measu...
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Keywords:
control study;
flow control;
duct using;
passive flow ... See more keywords