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Michalke, Alfons (1970) A Wave model for Sound Generation in Circular Jets. DLR-Forschungsbericht. Deutsche Forschungs-und Versuchsanstalt für Luft- und Raumfahrt. 31 S.
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Abstract
A wave model is used for the investigation of sound generation in circular jets. The source term of the Lighthill equation is expressed by a Fourier series in the azimuthal angle, is Fourier-transformed with respect to time, and each component is assumed to be of wave-type in jet direction. A far-field solution for the sound pressure is derived in this way for single azimuth-frequency components. It is found that the sound field depends strongly on a convection parameter and on a jet thickness parameter. The influence of axisymmetric and azimuthal source components is discussed. For a special source term with arbitrarily chosen amplitude distribution the convection factor and the jet thickness factor of sound intensity are calculated and discussed. The influence of the amplitude distribution of the source components is found to be of minor importance.
| Item URL in elib: | https://elib.dlr.de/63062/ | ||||||||
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| Document Type: | Monograph (DLR-Forschungsbericht) | ||||||||
| Title: | A Wave model for Sound Generation in Circular Jets | ||||||||
| Authors: |
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| Date: | November 1970 | ||||||||
| Open Access: | Yes | ||||||||
| Number of Pages: | 31 | ||||||||
| Publisher: | Deutsche Forschungs- und Versuchsanstalt für Luft-und Raumfahrt, e.V. | ||||||||
| Series Name: | Deutsche Luft- und Raumfahrt Forschungsbericht | ||||||||
| ISSN: | 0939-2963 | ||||||||
| Status: | Published | ||||||||
| Keywords: | jet noise, sound generation, wave model, circular jet | ||||||||
| Institution: | Deutsche Forschungs-und Versuchsanstalt für Luft- und Raumfahrt | ||||||||
| Department: | Institut für Turbulenzforschung | ||||||||
| HGF - Research field: | Aeronautics, Space and Transport | ||||||||
| HGF - Program: | other | ||||||||
| HGF - Program Themes: | other | ||||||||
| DLR - Research area: | Aeronautics | ||||||||
| DLR - Program: | L - no assignment | ||||||||
| DLR - Research theme (Project): | L - no assignment (old) | ||||||||
| Location: | Berlin-Adlershof | ||||||||
| Institutes and Institutions: | Institute of Propulsion Technology > Engine Acoustic | ||||||||
| Deposited By: | Michel, Prof. Dr.-Ing. Ulf | ||||||||
| Deposited On: | 08 Feb 2010 08:55 | ||||||||
| Last Modified: | 31 Jul 2019 19:27 |
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