Effect of serrated trailing edges on aerofoil tonal noise
Author:
Abstract
Publisher
Cambridge University Press (CUP)
Subject
Mechanical Engineering,Mechanics of Materials,Condensed Matter Physics
Reference34 articles.
1. Effect of spanwise domain size on direct numerical simulations of airfoil noise during flow separation and stall
2. On the universal trends in the noise reduction due to wavy leading edges in aerofoil–vortex interaction
3. Aerofoil tones at moderate Reynolds number
4. Discrete tones of isolated airfoils
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