The scattering of vorticity waves by an infinite cascade of flat plates in subsonic flow

DOI10.1016/0165-2125(93)90075-QzbMath0806.76030MaRDI QIDQ1329714

N. Peake

Publication date: 16 February 1995

Published in: Wave Motion (Search for Journal in Brave)

zbMATH Keywords

matchingWiener-Hopf techniquearbitrary reduced frequencyduct-mode coefficientsleading-edge regionlift distributiontrailing-edge region

Mathematics Subject Classification ID

General aerodynamics and subsonic flows (76G25) Hydro- and aero-acoustics (76Q05)

Related Items (3)

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

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• Zum Dirichlet-Problem der Helmholtzschen Schwingungsgleichung für ein gestaffeltes Streckengitter
• Zum Neumann-Problem der Helmholtzschen Schwingungsgleichung für ein gestaffeltes Streckengitter
• The interaction between a high-frequency gust and a blade row
• Unsteady Flow in a Supersonic Cascade with Subsonic Leading-Edge Locus
• Sound transmission through blade
• On the transmission of sound waves through a blade row
• The reflection of an electromagnetic plane wave by an infinite set of plates. II
• The reflection of an electromagnetic plane wave by an infinite set of plates. I
• The reflection of an electromagnetic plane wave by an infinite set of plates. III

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