Prediction of Non-Cavitation Propeller Noise in Time Domain
The blade frequency noise of non-cavitation propeller in a uniform flow is analyzed in time domain. The unsteady loading (dipole source) on the blade surface is calculated by a potential-based surface panel method. Then the time- dependent pressure data is used as the input for Ffowcs Williams-Hawki...
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Published in | China ocean engineering Vol. 25; no. 3; pp. 531 - 538 |
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Main Author | |
Format | Journal Article |
Language | English |
Published |
Heidelberg
Chinese Ocean Engineering Society
01.09.2011
The Ministry of Education Key Laboratory of High Speed Ship Engineering, Wuhan University of Technology, Wuhan 430033, China%College of Naval Architecture and Power, Naval University of Engineering, Wuhan 430033, China College of Naval Architecture and Power, Naval University of Engineering, Wuhan 430033, China |
Subjects | |
Online Access | Get full text |
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Summary: | The blade frequency noise of non-cavitation propeller in a uniform flow is analyzed in time domain. The unsteady loading (dipole source) on the blade surface is calculated by a potential-based surface panel method. Then the time- dependent pressure data is used as the input for Ffowcs Williams-Hawkings formulation to predict the acoustics pressure. The integration of noise source is performed over the true blade surface rather than the nothickness blade surface, and the effect of hub can be considered. The noise characteristics of the non-cavitation propeller and the numerical discretization forms are discussed. |
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Bibliography: | YE Jin-ming XIONG Ying XIAO Chang-run and BI Yi ( a College of Naval Architecture and Power, Naval University of Engineering, Wuhan 430033, China b The Ministry of Education Key Laboratory of High Speed Ship Engineering, Wuhan University of Technology, Wuhan 430033, China) 32-1441/P propeller; surface panel method, noise; time domain The blade frequency noise of non-cavitation propeller in a uniform flow is analyzed in time domain. The unsteady loading (dipole source) on the blade surface is calculated by a potential-based surface panel method. Then the time- dependent pressure data is used as the input for Ffowcs Williams-Hawkings formulation to predict the acoustics pressure. The integration of noise source is performed over the true blade surface rather than the nothickness blade surface, and the effect of hub can be considered. The noise characteristics of the non-cavitation propeller and the numerical discretization forms are discussed. ObjectType-Article-1 SourceType-Scholarly Journals-1 ObjectType-Feature-2 content type line 23 |
ISSN: | 0890-5487 2191-8945 |
DOI: | 10.1007/s13344-011-0043-4 |