Study of aerodynamic noise from UAV rotor in hover and forward flight
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DOI: 10.1088/1402-4896/adb5d2
Abstract: This study employed the Delayed Detached Eddy Simulation (DDES) turbulence model and the Ffowcs Williams-Hawkings (FW-H) acoustic analogy method to investigate the flow field and acoustic characteristics of a 1045 Unmanned Aerial Vehicle (UAV) rotor… read more here.
Keywords: forward flight; uav rotor; hover forward; noise ... See more keywords