An algorithm for the evaluation of the retarded configuration of a supersonic rotating surface has been developed, implemented and validated. This algorithm has been now used to test the capabilities of the Kirchhoff-Ffowcs Williams Hawkings formulation in the HSI noise prediction. Like the Kirchhoff approach, this method avoids the computation of the nonlinear three-dimensional terms and performs the integration on a (fixed or rotating) surface imcluding the noise-radiating body. Numerical results are presented and discussed.

Noise Prediction of High-Speed Rotating Blades Through the Kirchhoff-Ffowcs Williams Hawkings Formulation

Sandro IANNIELLO
1999

Abstract

An algorithm for the evaluation of the retarded configuration of a supersonic rotating surface has been developed, implemented and validated. This algorithm has been now used to test the capabilities of the Kirchhoff-Ffowcs Williams Hawkings formulation in the HSI noise prediction. Like the Kirchhoff approach, this method avoids the computation of the nonlinear three-dimensional terms and performs the integration on a (fixed or rotating) surface imcluding the noise-radiating body. Numerical results are presented and discussed.
1999
Istituto di iNgegneria del Mare - INM (ex INSEAN)
Inglese
Proceedings 5th AIAA/CEAS Aeroacoustics Conference
Fifth AIAA/CEAS Aeroacoustics Conference
http://arc.aiaa.org/doi/pdf/10.2514/6.1999-1930
10-12 May 1999
Greater Seattle - USA
Aeroacoustics
2
none
Catalano, Pietro; Ianniello, Sandro
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/20.500.14243/210524
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