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The interaction between a steady jet flow and a supersonic blade tip - MaRDI portal

The interaction between a steady jet flow and a supersonic blade tip

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Publication:4694473

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DOI10.1017/S0022112093000904zbMath0789.76079MaRDI QIDQ4694473

Publication date: 13 June 1994

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

zbMATH Keywords

radiation delta-function tip vortex total lift airfoil corner rigid airfoil semi-infinite-span airfoil side edge

Mathematics Subject Classification ID

Hydro- and aero-acoustics (76Q05) Supersonic flows (76J20)

Related Items (3)

Canonical sound fields in the frequency-domain theory of supersonic leading-edge noise ⋮ The scattering of vorticity waves by a supersonic rectangular wing ⋮ Basic singular fields in the theory of impulsive supersonic leading-edge noise

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