Using a time domain method based on the Ffowcs Williams-Hawkings equation, a reliable explanation is provided for the origin of singularities observed in the numerical prediction of supersonic propeller noise. In the last few years Tarn and, more recently, Amiet have analyzed the phenomenon from different points of view. The method proposed here offers a clear interpretation of the singularities based on a new description of sources, relating to the behaviour of lines where the propeller blade surface exhibits slope discontinuity.

On the possibility of singularities in the acoustic field of supersonic sources when BEM is applied to a wave equation

DE BERNARDIS Enrico;
1990

Abstract

Using a time domain method based on the Ffowcs Williams-Hawkings equation, a reliable explanation is provided for the origin of singularities observed in the numerical prediction of supersonic propeller noise. In the last few years Tarn and, more recently, Amiet have analyzed the phenomenon from different points of view. The method proposed here offers a clear interpretation of the singularities based on a new description of sources, relating to the behaviour of lines where the propeller blade surface exhibits slope discontinuity.
1990
Istituto di iNgegneria del Mare - INM (ex INSEAN)
Inglese
Annigeri B.S.; Tseng K.
Boundary Element Methods in Engineering (Proc. Int. Symp. on Boundary Element Methods: Advances in Solid and Fluid Mechanics)
International Symposium on Boundary Element Methods: Advances in Solid and Fluid Mechanics
522
528
7
978-3-642-84240-5
http://link.springer.com/chapter/10.1007/978-3-642-84238-2_66
Springer-Verlag
Berlin Heidelberg
GERMANIA
2-4 Ottobre 1989
East Hartford, Connecticut (USA)
Acoustics
Boundary Element Method
Supersonic Source
2
reserved
DE BERNARDIS, Enrico; Farassat, Fereidoun
273
info:eu-repo/semantics/conferenceObject
04 Contributo in convegno::04.01 Contributo in Atti di convegno
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Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/20.500.14243/219111
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