Regimes of tonal noise on an airfoil at moderate Reynolds number
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Publication:2796614
DOI10.1017/JFM.2015.475zbMath1382.76150OpenAlexW2296694989MaRDI QIDQ2796614
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Publication date: 29 March 2016
Published in: Journal of Fluid Mechanics (Search for Journal in Brave)
Full work available at URL: https://doi.org/10.1017/jfm.2015.475
Boundary-layer theory, separation and reattachment, higher-order effects (76D10) General aerodynamics and subsonic flows (76G25) Viscous vortex flows (76D17)
Related Items (6)
Transition, intermittency and phase interference effects in airfoil secondary tones and acoustic feedback loop ⋮ Transition in a separation bubble under tonal and broadband acoustic excitation ⋮ Influence of a weak adverse pressure gradient on the generation of tonal protuberance noise in a laminar boundary layer ⋮ Effect of serrated trailing edges on aerofoil tonal noise ⋮ A complementary numerical and experimental study of the influence of Reynolds number on theoretical models for wingtip vortices ⋮ A secondary modulation mechanism for aerofoil tonal self-noise generation
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