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Published in 2019 at "Journal of The American Helicopter Society"
DOI: 10.4050/jahs.65.012007
Abstract: In this study, hover acoustic measurements are taken on isolated rotor-airframe configurations representative of smallscale, rotary-wing unmanned aircraft systems (UAS). Each rotor-airframe configuration consists of two fixed-pitch blades powered by a brushless motor, with a…
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Keywords:
rotor;
rotor airframe;
rotary wing;
noise ... See more keywords