This paper investigates the effect of blade skew on the interaction tones produced by a contra-rotating unmanned aerial vehicle rotor system using computational, analytical, and experimental methods. Computational fluid dynamics simulations are used to predict the periodic unsteady loading on the blades of three sets of rotors with different amounts of skew. This loading data is used to predict the acoustic pressure time-history and the sound pressure levels of the interaction tones radiated from the rotor systems. The predictions are compared with experimental measurements and show good agreement. It is observed that the amplitude of prominent interaction tones decreases as the blade skew angle increases and that the overall A-weighted sound power level of the interaction tones radiated from the rotor systems decreases significantly as skew angle increases. It is shown that this reduction in noise level is in-part caused by the de-phasing of the acoustic pressure emitted from different radii along the blades of the rotor systems.
Read full abstract