Asymptotic theory of supersonic propeller noise

DOI10.2514/3.11978zbMath0798.76082OpenAlexW3021578371MaRDI QIDQ4292292

Edmane Envia

Publication date: 1 June 1994

Published in: AIAA Journal (Search for Journal in Brave)

Full work available at URL: http://hdl.handle.net/2060/19930014881

zbMATH Keywords

large-blade-count approximationLighthill quadrupole sourcepeak sound pressure levelradiation efficiency integrals

Mathematics Subject Classification ID

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

Related Items (3)

Development of immersed boundary computational aeroacoustic prediction capabilities for open-rotor noise ⋮ Acoustic theory of the many-bladed contra-rotating propeller: analysis of the effects of blade sweep on wake interaction noise ⋮ Acoustic theory of the many-bladed contra-rotating propeller: physics of the wake interaction noise critical sources

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