The scattering of vorticity waves by a supersonic rectangular wing

DOI10.1016/S0165-2125(97)00005-XzbMath0921.76154MaRDI QIDQ1276598

N. Peake

Publication date: 6 October 1999

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

zbMATH Keywords

analytical solutionacoustic energyfar-field radiationfinite chordfinite spanlarge gust sweep anglesmodified Wiener-Hopf techniqueunsteady lift

Mathematics Subject Classification ID

Scattering theory for PDEs (35P25) Hydro- and aero-acoustics (76Q05) Supersonic flows (76J20)

Related Items (1)

Canonical sound fields in the frequency-domain theory of supersonic leading-edge noise

Cites Work

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• Aerodynamic theory for wing with side edge passing subsonically through a gust
• Sound generated from the interruption of a steady flow by a supersonically moving aerofoil
• Acoustic radiation from an airfoil in a turbulent stream
• The unsteady lift on a swept blade tip
• The interaction between a steady jet flow and a supersonic blade tip
• The two-dimensional sound field due to a pair of interacting compliant pistons
• The oscillating rectangular airfoil at supersonic speeds

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