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A Computational Study on the Aeroacoustics of a Multi-Rotor Unmanned Aerial System (open access)

A Computational Study on the Aeroacoustics of a Multi-Rotor Unmanned Aerial System

Article studying the noise generated by a quadrotor biplane unmanned aerial system (UAS) for various conditions in terms of the UAS pitch angle, propellers rotating velocity (RPM), and the UAS speed to understand the physics involved in its aeroacoustics and structure-borne noise.
Date: October 18, 2021
Creator: Heydari, Morteza; Sadat Hosseini, Seyed Hamid & Singh, Rajneesh
System: The UNT Digital Library