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A Numerical Approach to Possible Identification of the Noisiest Zones of a Wall Surface with a Flow Interaction
- Source :
- Open Journal of Fluid Dynamics. :525-545
- Publication Year :
- 2017
- Publisher :
- Scientific Research Publishing, Inc., 2017.
-
Abstract
- This paper examines the use of proper orthogonal decomposition (POD) and singular value decomposition (SVD) to identify zones on the surface of the source that contribute the most to the sound power the source radiates. First, computational fluid dynamics (CFD) is used to obtain the pressure field at the surface of the blade in a subsonic regime. Then the fluctuation of this pressure field is used as the input for the loading noise in the Ffowcs Williams and Hawkings (FW&H) acoustic analogy. The FW&H analogy is used to calculate the sound power that is radiated by the blade. Secondly, the most important acoustic modes of POD and SVD are used to reconstruct the radiated sound power. The results obtained through POD and SVD are similar to the acoustic power directly obtained with the FW&H analogy. It was observed that the importance of the modes to the radiated sound power is not necessarily in ascending order (for the studied case, the seventh mode was the main contributor). Finally, maps of the most contributing POD and SVD modes have been produced. These maps show the zones on the surface of the blade, where the dipolar aeroacoustic sources contribute the most to the radiated sound power. These identifications are expected to be used as a guide to design and shape the blade surface in order to reduce its radiated noise.
- Subjects :
- Physics
business.industry
Acoustics
Flow (psychology)
Mode (statistics)
Aerodynamics
Computational fluid dynamics
Sound power
01 natural sciences
010305 fluids & plasmas
Physics::Fluid Dynamics
010101 applied mathematics
Noise
0103 physical sciences
Singular value decomposition
Aeroacoustics
0101 mathematics
business
Subjects
Details
- ISSN :
- 21653860 and 21653852
- Database :
- OpenAIRE
- Journal :
- Open Journal of Fluid Dynamics
- Accession number :
- edsair.doi...........3836943a733fe454bb625c2a95fb9fdc