Noise reduction on low Reynolds number rotors by boundary layer transition

Author:

Gowree E.R.,Jaroslawski T.,Mellot B.,Gojon R.

Publisher

Elsevier BV

Subject

Acoustics and Ultrasonics

Reference32 articles.

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4. Prediction of noise from low Reynolds number rotors with different number of blades using a non-linear vortex lattice method, in;Jo;25th AIAA/CEAS Aeroacoustics Conference,2019

5. R. Serré, H. Fournier, J. Moschetta, A design methodology for quiet and long endurance MAV rotors, Int. J. Micro Air Veh. 11.

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