The interaction between a high-frequency gust and a blade row

DOI10.1017/S0022112092002039zbMath0754.76083OpenAlexW2039931203MaRDI QIDQ4014062

N. Peake

Publication date: 4 October 1992

Published in: Journal of Fluid Mechanics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1017/s0022112092002039

zbMATH Keywords

Wiener-Hopf techniqueasymptotic analysisunsteady liftfinite-chord flat platesincident vorticity waveinfinite cascade

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25) General theory of rotating fluids (76U05) Fourier and Fourier-Stieltjes transforms and other transforms of Fourier type (42A38)

Related Items (6)

The scattering of vorticity waves by an infinite cascade of flat plates in subsonic flow ⋮ Three-dimensional effects of cascade perforations on rotor–stator interaction noise ⋮ On the flow-acoustic coupling of fan blades with over-the-rotor liner ⋮ An analytic solution for gust–cascade interaction noise including effects of realistic aerofoil geometry ⋮ On a uniformly valid analytical rectilinear cascade response function ⋮ Three-dimensional effects in cascade-gust interaction

Cites Work

• Zum Dirichlet-Problem der Helmholtzschen Schwingungsgleichung für ein gestaffeltes Streckengitter
• Zum Neumann-Problem der Helmholtzschen Schwingungsgleichung für ein gestaffeltes Streckengitter
• Sound transmission through blade
• Acoustic beaming and reflexion from wave-bearing surfaces
• On the transmission of sound waves through a blade row

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